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ADOAG89 279 GENERAL ELECTRIC CO LYNN MA AIRCRAFT ENGINE GROUPF F/6 11/5 MARITIME PATROL AIRCRAFT ENGINESTUDY. GENERAL ELECTRIC O*tIVAT--ETC(U) APR 79 R NIRSCHKRON. R N DAVIS, R E WARREN N6226976C-0414 UNLASFIE 79AE052V0-3 NADC-79133-6O-VOL-3 L UmhEEAhhhED
83

UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

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Page 1: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

ADOAG89 279 GENERAL ELECTRIC CO LYNN MA AIRCRAFT ENGINE GROUPF F/6 11/5

MARITIME PATROL AIRCRAFT ENGINE STUDY. GENERAL ELECTRIC O*tIVAT--ETC(U)APR 79 R NIRSCHKRON. R N DAVIS, R E WARREN N6226976C-0414

UNLASFIE 79AE052V0-3 NADC-79133-6O-VOL-3 LUmhEEAhhhED

Page 2: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*~ 11112051111112-

11111 1.5111111.6

MtrROCOPY R( SO~LONON HfS CHAR INArNAl 1III All Ol IANWAI,':4.; A

Page 3: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

0

Page 4: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

'77

I UnclassifiedSECURITY CLASIFICATION 0F THIS PAGE (Wh., no##. xnee,#dj ________________

READ INSTRUCTIONSREPORT DOCUMENTATION PAGE BEFORE COMPLETING FORMI . REPOINT HUNGER 12 GOVT ACCESSION NO, 3. RECIPIENT'S CATALOG NUMBER

NADCd-79133-60 ________

14. TITLE (ovid &.AtifD.) S. TYPE OF REPORT 6 PERIOD COVEREDt Maritime Patrol Aircraft Engine Study- Final ReportGeneral Electric Derivative Engines; Oct. 1978-Apr. 1979Volume III, Appendix B--Performance 6. PERFORMING ONG. REPORT NUMBER

Dat -DF4T tdyA ub~ R79AEG052 %,--* 7. AUTHORI.) 6. CONTRACT OR GRANT MUMUERi'a)

R.Ircko N62269-78-C-044

9. PERFORMING ORGANIZATION NAME AND ADDRESS 10. PROGRAM ELEMENT. PROJECT. TASK

Aircraft Engine Group 7-A03P-O3PAWOlE/7W880-001;Lynn, Massachusetts 01910 ltbrk Unit XG4201.

It. CONTROLLING OFFICE NAME ANO ADDRESS 12. REPORT DATE

30 April 1979Naval Air Development Center 13 NUMBER OF PAGESI Warminster, Pennsylvania 18974 801. MONITORING AGENCY NAME & AOORESS(Of d"ll....' Ur~. (*o,trolion Olliee) IS. SECURITY CLASS. (of Ohio Popoff)

UnclassifiedT.OECLASSIFrICATION.'DOWNGRADINOG

SCHEDULE

IS. DISTRIBUTION STATEMENT (of MOP. R~p.te

Approved for public release, distribution unlimited.

17. DISTRIBUTION STATEMENT (of she obatFm1 ..,I.,d In, 910CA 20. it diUfn ra. Re tpoft)

* III. SUPPLEMENTARY NOTES

IS. KEY WORDS (Coqwtimwe -,, of. f roe eIt"eatoy nag fdfnfifr 6v 61.,eh n.umb"t)

3Aircraft Propulsion Turbofan Engine* 1 IDerivative Engine Turboshaft Engine

Maritime Patrol Aircraft .Turboprop Engine

20 ABS7i47 I(Co~oa n owosd tM.00rIn d~frh it ob

- ~ "his study developed data on General Electric common* core derivative engines for use irn Maritime Patrol Aircraft* CMPA) concept formulation studies. The study included the

screening of potential General Electric turbofan andI turboprop/turboshaft engines and the preparation of technicaDD Fjo"N71 1473 EDITION OF I'NOV 65 IS OSSOLETF Un la siie

* 3 SECURITY CLASSIFICATION OF TNIS PAGR fUwia 005 Or~io*

Page 5: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

Unclassified29CUOUTY CLA8IPICAVSON OF THIS PAGS~U a... ROW04

and planning information on three of the most promising engine

candidates. Screening of General Electric derivative candidates*was performed utilizing an analytical MPA model using

synthesized mission profiles to rank the candidates in terms offuel consumption, weight, cost and complexity. The threeturboprop engines selected for further study were as follows:TF34 growth derivative version with boost and new LPT (TF34/T7Study Al), F404 derivative with booster stages and new LPT

I "(F404/Tl Study Al), and GE27 scaled and boosted study engine(GE27/T3 Study Al). Volume I summarizes the screening analysisand contains technical, planning, installation, cost anddevelopment data for the three selected turboprop engines.Volumes II, III and IV of this report contain the detailedperformance data estimates for the GE27/T3 Study Al, TF34/T7Study Al and F404/Tl Study Al turboprop engines, respectively.

I

-X -ceasson ForI -Dr;,C TAB

SItC

.

i -. iJUne Im f &Aii gCUMTYV CLAWPICASON OF TIS PA@Oa~. D R. b-

Page 6: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

GENERAL@EETI

TECHNICAL INFORMATION SERIESTitle Palo

VOLUME IIIAUT600A suDjacT

R. Hirschkron NP RPLINSUY R79AEG052R. E. Warren FINAL REPORT 4/26/79TITLE 6.L CLASS 3 [email protected] U S. CLASS

MPA PROPULSION STUDY - FINAL REPORT sow *c-AS

COPIES AVAILANLE FROM 0PAE

AEG TECHNICAL INFORMATION CENTER 801LYNN 24001 QEVENDALE N-32

SUMMIARY .E CLAss 3 SOV? CLASS Unclassified

Turboshaft performance and economic dataiprovided for three engines to report

Maritime Patrol Aircraft (MPA) studies beingcarried out by airframe companies under USNcontract. The three engines are the GE27/T3Study Al, an advanced 8000 SHP engine, theI TF34/T7 Study Al, an 9500 SHP derivative of agrowth TF34 engine and the F404/Tl Study Al, aturboshaft derivative of the F404 turbofanj engine in the 12500 SHP class.

5 MPA, GE27/T3 Study Al, TF34/T7 Study Al,

F404/Tl Study Al, Turboprop, Turboshaft

CONTRACT NUMBER N62269-78-C-0414- SPONSORING ORGANIZATION U * S * Navy

APPROVED BY R. E. Neitzel e~, zLynn Preliminary DesignIAUTHOR'S MANASENI) 40ft5A"l ZATION)

DEFT./OPE RATION AE&TPD LOCATION Lynn, Mass.

AIRCRAFT ENGINE GROUP

U DV 217

Page 7: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

R7 9AEGO52

* I MPA PROPULSION STUDY

g FINAL REPORT

APPENDIX B -TF34/T7 STUDY Al PERFORMANCE DATA

ii (IN FOUR VOLUMES)

by

I R. HirschkronR. H. Davis

I R. E. Warren

April 26, 1979

Prepared for U. S. Navy under Contract N62269-78-C-0414

H :.....

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I

APPENDIX B

The performance data contained in this appendix is for

the TF34/T7 Study Al engine. Tables are included which define

the flight conditions and operating points, nomenclature and

station designations.

All data is uninstalled and is based on a fuel heating

I value of 18400 Btu/lbm.

tiI

III

Ii

I

- . - _II I I

Page 9: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

APPENDIX B

TF34 /T.7STUDY Al

RAM RECOVERY =1, CUSTOMER BLEED =0, POWER EXTRACTION =0

jCase No. Alt. MO Day Power Setftns

1-6 0 0 STD max, IRPMC, Part PowerI7-12 0 .113-18 0 .219-24 0 .3 I25-30 0 0 HOT31-36 0 .137-42 0 .243-48 0 .3

495 0. STD :lRp ~Part ,Power

5 9-63 0 .6564-8 0K .7

85-89 5K .390-94 5K .495-99 SK .5100-104 5K .6105-109 10K .110-114 10K .3Ii115-119 10K .4

120-124 10K .5

140-144 10K .8145-149 15K .3150-154 15K .4 *

155-159 15K .5I160-164 15K .6165-i69 15K .7170-174 15K .751175-179 15K .8180-184 20K .4 STD185-189 20K .519-9IZK.190-194 20K .6

Page 10: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

APPENDIX B

I Case No. Alt. Mo RAM Power Settings

200-204 20K .75 STD IRP MC, Part Power205-209 20K .8Z10-214 25K .4215-219 25K .5220-224 25K .6225-229 2SK .7230-234 25K .75235-239 25K .8240-244 30K .4

245-249 30K .5250-254 30K .6255-259 30K .7260-264 30K .75Z65-269 30K .8270-274 35K .5275-279 35K .6280-284 35K .7285-289 35K .75290-294 35K .8295-299 40K .5300-304 40K .6305-309 40K .7310-314 40K .75315-319 40K .8320-324 45K .5

325-329 45K .6330-334 45K .7

335-339 45K .75340-344 45K .8S345 00 TROP MAX

,L I

Page 11: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

-l - *-- ....

APPENDIX B NOMENCLATURE

SYMBOL DESCRIPTION UNITS

CASE Numerical data point identification

ALT Geopotential pressure altitude ft

XM Flight Mach number

ERAMI Inlet ram recovery

WB3Q Customer air bleed (fraction of WI)

PAMB Ambient pressure psia

TAMB Ambient temperatures OR

DTAMB Deviation from standard ambient temperature OF(ambient minus standard temperature)

P2 First compressor inlet total pressure psia

T2 First compressor inlet total temperature OR

PWSD Output shaft horsepower, delivered hp

SFC Specific fuel consumption (WFT/PWSD) Ibm/hr/hp

EPWSD Equivalent output shaft horsepower, delivered hp

ESFC Equivalent specific fuel consumption (WFT/EPWSD) ibm/hr/hp

WFT Fuel flow rate ibm/hr

FN Net thrust (in axial direction) lbf

W1 Engine inlet airflow rate Ibm/sec

WIR Referred engine inlet airflow rate ibm/sec

W2R Referred booster inlet airflow rate Ibm/sec

P21Q2 Booster pressure ratio

' ECL Booster adiabatic efficiency

W25R Referred compressor inlet airflow rate ibm/sec

I P3Q25 Compressor pressure ratio

ECH Compressor adiabatic efficiency!

.1 5

Page 12: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

IAPPENDIX BSYMBOL DESCRIPTION UNITS

PB3 Compressor discharge air bleed pressure psia

I TB3 Compressor discharge air bleed temperature OR

EB Combustor efficiency

T41 HP turbine rotor inlet temperature OR

DH41R HP turbine referred energy function Btu/lbm/OR

P41Q42 HP turbine pressure ratio

ETH HP turbine adiabatic efficiency

I T47 LP turbine rotor inlet temperature OR

DH47R LP turbine referred energy function Btu/lbm/°R

I P47Q5 LP turbine pressure ratio

ETL LP turbine adiabatic efficiency

XNL LP turbine rotor speed (output shaft speed) rpm

GW3S42 Ratio of parasitic flow originating at station

3 and reentering at station 42 to compressorinlet flow.

GW3S49 Ratio of parasitic flow originating at station3 and reentering at station 49 to compressori inlet flow.

GW2742 Ratio of parasitic flow originating at station27 and reentering at station 42 to compressorinlet flow.

GW2749 Ratio of parasitic flow originating at station27 and reentering at station 49 to compressorinlet flow.

GWLK3 Ratio of overboard leakage flow from stationi 3 to compressor inlet flow.

GHW27 Enthalpy fraction at station 27, (H27-H25)/(H3-H25)-

, PWPAR High pressure rotor parasitic power hp

* P2125Q Inter-compressor pressure loss

P3D4lQ Combustor pressure loss

I P4247Q Inter-turbine pressure loss

P5D8Q Exhaust system pressure loss

Iiiti O

Page 13: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I APPENDIX B

SYMBOL DESCR1PTION UNITS

CD8 Exhaust nozzle flow discharge coefficient

Cv8 Exhaust nozzle velocity coefficient

A8 Exhaust nozzle area sq. in.

P8QAMB Exhaust nozzle pressure ratio

T8 Exhaust gas temperature O

W8 Exhaust gas flow rate ibm/sec

P8 Exhaust gas pressure PS ia

Page 14: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

4 4 J J

0 0 C

1U)~U V-H

-E-4

90 -H . li r4 "

E-, E- -4 - 4 d

Q4 M s:4

E4,0-d4

2~~r -- 4)~*to H___ 0 P444.1

Wb -d V J-

-4 a)' 4 t

04 m 0604

t" 0 )

W m0.(

Page 15: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

.' TF34/T7 STUDY At **ESTIMATED PERFORMANCE LyNN MASS. APRIL l6, 1979

CASE 1.000 2.0000 3.0000 4.0000 5.0000 6.0000

ALT 0. 0. 0. 0. 0 0..M 0, 0, 0 0. 06- 0,

ERAMI 1.0000 1.0000 laooo 1,0000 1.0000 1.0000WB3Q 0. 0. O. 0. 0. 0,

PAMB 14,.696 14.696 14j696 14.696 14,696 14,696TAMB 515.67 516.67 SIB..67 518.67 S169? 5156b7P2 14.69b 19.696 14.696 14,696 14,696 14,696T2 S18.67 518.67 518.67 518.67 518.67 518.67PiSD 9536W3 eas5.9 7S32.2 3681. 368,b 2481,3,EPWSD 10129.3 8758.1 7981.8 5989.6 4060.6 2619.1SFC 0.4216 0,43t2 0;4392 0.4660 0,5057 0,5783ESFC 0.4061 0.4067 0.4144 0.4420 0.4831 0.5478vJFT 4021,0 3561.7 3308,1 2647.5 1961.S 1434,8FN 1482.52 1245.50 1124.'1 769,53 512.56 344.S9Wl 52,088 48.023 45,793 38,643 32.316 27.136XNL 11827. 11827. 11827. 10420. 8719o 7508.P83 329.36 298.98 282.37 228,90 183.34 14*6.97TB3 1400.6 1361.6 1340.4 1259.9 1179.7 1108.SP8 17.354 16.907 16.681 16.041 15.576 15.287TO 1509.3 1484,9 1470.6 1399.7 1335.3 1267,7

I.

I

I

I• !

Page 16: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY At **ESTIMATED PERFORMANCE LYNN MASS. APRIL 26v 5979

I CASE 7.0000 6,0000 9.0000 10.0000 11,0000 12,0000

ALT O. 0. 0. O 0. 0.

x 0.1000 0.0 1000

ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000 1,00003 O. 0. . O. O. 0.

PANS 14.696 14,696 14.696 14.696 14.696 14,696TANS 518.6? 518.67 518.7 516,67 518067 518.67P2 14,799 14.799 14.799 14,799 14,799 140799

. 12 519.71 519.71 519.71 S19.71 519.71 519,71PW$D 9581.6 8294.4 7565.9 5718.4 3882.4 2502.9EPWSD 9914,3 8570'5 7813.0 5831.4 3985#4 2567.5SFC 0.4206 0.303 0.4381 0.4643 0.5067 0.57S2ESFC 0.4065 004164 0:4243 0.4514 0.4936 OSbO7NFT 4030.0 3568,7 3314.9 2654.9 1967.3 1439,6FN 1310,47 1087,68 973.20 642.,o2 405.98 254.63NI 5.229 48,143 45.912 38,780 32,443 27028XNL 11827. 11827. 11827. 10407. 8711. 7S06.PB3 330.25 299.72 283.10 229.72 184.07 147.63T53 140103 1362,4 1341.? 12009 1180.9 1109.7P8 17.36 16.919 16.691 16,049 15.S83 150292T8 1508.-S 1484.3 1469.9 139S.6 1334.2 1266.6

11

I

Page 17: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I1

** TF34/T? STUDY Al **_-. ESTIMATED PERFURMANCE LYNN MASS, APRIL 26, 1979

CASE 13.0000 14.0000 15.0000 16.0000 17.0000 18.0000

ALT 0, 0. 0. 00 0. 0.X M 0.000 0 * 0 00-2000 8.200, 002000 002000ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000 100000W83Q 0. 0. 0 00 0.

.PAMS 14,496 140696 14 --66 14bq6 14e696 14696STAMB 51s067 S16,67 5t8067 516067 51867 St6,67

PZ 15.112 156112 15.111 15.112 IS112 tS.112T2 522e83 522.63 S22,83 522w83 522.83 522,83PWSD 9703A8 840343 76S.62 5829.2 3963.0 2568.5[PWSD 10287.5 8879.6 8089.4 6094.3 4117.6 26S3.58FC 0,4178 0,4273 0.4350 014S94 0.5006 0,5661ES[C 0.3941 0.4044 0.4123 004394 0.4020 0.5480WFT 4054.3 3590.6 3335.3 2677.9 1984.6 1454.1IN 1149.80 936.24 829071 522.03 304044 167.47Wt 52,602 48520 4.266 39.211 32.825 270b6XNL 118270 11827, 11827. 1o374 8688,1 7S03.P83 332.62 302.07 265.29 232.27 16923 149.61T83 1403.1 1364.9 1343.5 1264.2 1184.4 11131P8 170401 169949 16,716 160074 1SbOS 15.305r8 1506.9 1482.3 1468,0 1395o4 1331.1 12633

i L ...

I

Page 18: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I- ESIMATD **TF341TY STUDY AltESTMAEDPERFORMANCE LYNN MASS, APRIL 26o 19?9

CASE 19.0000 20.0000 21.0000 22,0000 23.0000 2400000

A40 0 ~ 0~ 0 0. 0 * 0.X14 0.3000 003000 0.3000 0.3000 0,3000 0.3000ERAt4I 1.0000 169000 1;0000 1,0000 1.0000 160000W53Q 0. 0. 00 ol 0. 0.PANS 14,496 14,696 14,:696 140696 140696 l4*696YAMS 518.6? 516.67 518.67 518.6? 518.67 515,6702 I04 15,644 15.64 14~44 15,644 15.644 15.644T2 528.04 526104 528,04 528,04 526,04 564fPVISD 9693e2 8579.10 7833.0 6011.6D 4098.0 lb6.00EPWSD 10650.5 9164,3 83S9,8 63200b 0255.2 2738,5SFC 0.0135 0.4226 0,4299 0,4516 0,4913 0.5525sESFC 0.3841 003948 0.4028 014295 0.4731 0IS399WFT 4091*2 3615.6 3367,7 2714.7 2013.3 3478,4

-N 994.41 794.83 691.66 405.52 206.39 62*02Ni 530187 49.114 461840 39.904 33,463 26.24XNL 115270 118270 11827. 10302. 8646. 7497.

T63 1406.2 1368.7 1347,4 1269.4 1102 112&*5

pa1,5 702 107S 101 S64I65ToI0. 494 16,O t90 36t lse

Page 19: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I-** TF34/T7 STUDY Al *t

ESTIMATED PERFURMANCE LYNN MASS. APRIL 26, 1979

A S CAS,0012b,: 0000 27.0000 28.0000 29*0000 30.0000

ALT 0. o0 O. 0. 0, 0.xM 0. o. 0,. 0. 0ERAM! 1.0000 1.0000 1!0000 1.0000 100o0 190000WB3Q O. 0. 0O 0PAMB 14,696 14.696 14.696 14,696 14,696 14.696TAM S562.67 562,67 56;.17 562.467 S62b7 b,6PZ 14696 14.696 14.696 14.696 14,696 14.696

. . T 562.67 S62167 56267 562.67 S62.6? S62,67* PWSD 7061.3 6203.8 5769.0 4314.0 2618.1 1706.S

EPWSD 7461.0 6550.0 6090.0 4536.0 2965.0 1803.0.VC 0.4513 0.4615 0.#6bS OSOtS 0.5674 0,6763I [FC 0.4271 0.4371 0.4418 0.4770 0.5391 0.6400Wry 3t86oA 2862.9 2691.3 2163.5 1596.9 115,40.N 10404 869.28 804.,06 SSSW?T 369.56 243.48NI 41,725 39.242 37,979 32.261 2b,936 220283

.. XNL 11827. 11414o 11061, 9416. 60 2o 6936,- P63 263096 244.40 234.3t 191,26 152.95 120,86

T83 1417.4 138b.3 1366.6 12668 1209.2 1132.9I P8 160.52 16.212 16.09S I5655 15,324 ISlO

Ta 1569.5 1538,'5 1517.7 1447.3 1367.1 1325,4

i-

! I

'I-I

-. _ __ _ ___-_ _

Page 20: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/TT STUDY Alt*I- ESTIMATED PERFORMANCE LYNN MASS, APRIL 26o 1979

.-CASE 31.0000 52010000 33"9000 34.0'000 35'0000 3690000

ALT 0. 0. 0. 0. ow 0.-. K 0,1000 0.1000 0.10oo00 *1000 061008 0100

UERAMI 1:0000 1:0000 1:0000 1*0000 1.0000 190000W50 o : 00. 0w

3PAMB 14.6;96 14,b96 14.b99b 14,696 14*696 14*696T AMS 562.67 562.67 562.67 562,67 562.67 S62,67pa 14,79q 14,799 14,099 14,799 14,799 140799TZ 563.S 380 563.80 63, 0 563. S380 563.0IPWSD 7095.i9 6243-2 5605.6 4343.1 2040.3 1727.,6

-EPWSD 7322.09 6437.7 S963.8 4460.7 2914,0 1771.2SFC 0.402 0,6599 0.4649 00499S 0.5649 0.b?09

* IESFC 94362 0*44b0 0.4011 004864 G*5506 0.bS44__ FT 3194,3 287103 2699.0 2169.6 1604.4 1159.1

FN 858.62 735.84 674.16 444w82 279.00 164681NI 41,-849 39.388 38.117 32.083 27.0b4 22.41I____ X1L 11827. 11002. 11068. 9607* 8022. 694S,P83 264.74 245,31 235.16b 191.98 153.68 121.61

T 83 1418.1 1387.5 1369.8B 129000 1210.7 1134,6PS 16.463 16.224 16.104 150662 15.33? 15.108T& 1568.7 1537.3 1316.6 1446.2 138599 1323o6

Page 21: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T7 STUDY At *

I ESTIMATED PERFORMANCE LyN4 MASSo APRIL 26. 1979

- CASE 37.0000 38.0000 39.0000 40.0000 41.0000 42.0000

-ALT 0. 0., 0 0. 0. 0.EM 001000 0.2000 0.2o;0 002000 0.2000 0020o0ERAMI 100000 1.0000 1.0000 1.0000 1.0000 1.0000W839 0. 0. 0. 0. 0. 0.

--- PAMS 14.69b 14,'696 14.A96 14,69b 14,696 14.696*TAMS 562.67 562.67 562*'b7 562.67 5S62.67 S62.67

Pa 154A112 156112 1500112 13.112 15.112 I5.112TZ 567.16 56718 567.,16 567.1 567.16 567.18PWSD 71979~3 6361'5 5915.7 44310? 2911.2 1782.7EPWSO 7578.,9 6663.6 6207,4 4610.2 3010.,3 1631.3SFC 0.'4466 0.4552 0-4602 0.4937 0.5564 006574ESP'C 0.4241 0,4332 0:4385 0.4746 0.5360 016400

- ~ WFT 3214.5s 2695.6 2722.2 218?.9 1619.6 1172.0F71667 609o;31 551.70 337&,64 187.46 910.80

Ml 42,167 39.609 38.534 32.748 27,423 22.778XNL 11627. 11361. 11032. 9373w 8017. 6956.P93 266.87- 247o93 237.t73 194v15 133.71 123.54T83 1420.6 1390.6 1373.1 1293.6 3218.9 1139.5Pe 160468 l60Mq 164432 15.678 15.346 15.12716 1566.14 1533.8 1513.,3 1442.04 13621 1319.3

Page 22: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**TF34/TI STUDY Alt*

I- ESTIMATED PERFORMANCE LYNN MIASS, APRIL 26# 1919

CASE 43,0000 44.0000 450000 4b,0000 47,0000 48.0000

ALT 0o) o 0. 0. 0, 0.* K 00,3000 0.3000 0.3000 0,3000 0,3000 063000*ERAMI 160000 160000 1.0000 100000 100000 1*0000

W6830 0.69 o.69 00~ 6 0. 00PAM 1.69 tob6 1, 96 14,696 14.696 14.'b96I AMS 562.67 562.67 S62.b6 562.67 562.67 562,67

pa 15.,643 IS*643 IS.J643 15.643 15.643 15.64372 572.82 572,82 S12'ea 572so8l 572.82 97lqj63IPWBD 7369:00 6560:5s b098:3 4579:9 3020.4 1877:3

SFC 0.4408 0,4476 0;4S2$ 0,4844 0,S433 0,6356JESFC 0.4145 0.42?? 0,;4264 0,4656 oos29. 09631SWFT 3246,4. 2936.7 2761.1 2218.? 1609.3 1193.6

5N 89974 488.78 43b.98 234j.1? 10008 I15.94Il Ni 427% 40e525 39.23b 33.369 18.032 23*3S25 _ NL 11827. 11296. 10974. 9324o 6009. 6973.

Pas 270e47 252.37 2440SO 197.84 19.16 1ab G0TB3 142S,3 1396.3 1378.7 1299.7 1221.8 114;.5Pa 16.129 16.303 16.;190 15.712 ISOM7 15.6TS 1562.'6 15S261 1506. 1437.4 1376.2 1312.00

Page 23: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I ~ESTIMIATED PERFORMANCE LYNN MASS, PI 2,17

CASE 49*0000 50,0000 51.0000 52,0000 53,0000

ALT 0. 0. 0. 0. 00Em 0.4000 0.4000 0.4000 0,4000 0.4000ERAMt 100000 1.0000 1.0000 100000 1.0000

1WB39 000000TAMB 513.07 518.67 518.67? 516l 518.67Pa t6.410 16.410 16,410 16.41 16.410ITZ 535.33 535*33 53.33 535.33 535.33PW30S 8831.5 8095.8 6266.1 4296.6 2.260EPW3D 9497.6 86S. 6562'8 4400.7 2819.9I. FC 0.4162 0,4224 0f;4413 0,4780 0.5341ESFc 0.3870 0,3946 0s4214 0,466? 0.5)56NP? 3675.5 3419.5 2765.4 2053.8 1510.3FN b56;07 560.56 292.18 1020 07.90

l 993 470761 40,860 34.371 24111tXL 118?7. 11762. 10193. 8595. 7467.

P83 311.11 294.50 242,07 195.01 157.bb1 73 1374.2 1353.6 1276.5 1198.3 1127.8

PS 17.077 16.842 16.183 15.676 1593S9T& 147S.3 1459.6 1383,4 1318.8 1250.6

Page 24: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/~T? STUDY Alt[ ESTIMATED PERFORMANCE LYNN4 MASS. APRIL 26# 1979

ICASE 541.0000 55.0000 56,0000 57.0000 S6.0000

ALT 0. 0. 0. 0. 0.0X100 0.5000oso 0.5000 ,5000 0.5000

ERAMI 1.0000 100000 1.0000 1.0000 100000W839 0. 0. 0. 0. 0.IPAMS 14,696 14,69b 140.698 14.696 14,696TAMB 516.6? 518*67 518.6? 5 18.4W7 515.67P2 00.3S 1i.'43S 17/W-35 17.435 17.4135TZ5449b9 544.69 S44.:49 544w69 544*69

__ PW3D 9145.6 8470.8 6601.2 4547.2 3023.8EPWSD 9802,3 9021.7 6827.2 @551.4 2901*33FSC 0*4084 0.4124 0.4289 0.4630 0.5129

5E3FC 0.3810 0.3872 0,.4147 0.4825 0.5345WFT 3735,1 3493.2 2831.2 2105.1 1550.8

FN 517o42 433.97 178009 3.26 m9b*42wi t"02 4,D7 42424 35.536 30,232

*XNL 115270 11605. 1005b. 8525. 7470.P83 317.58 302.61 249,53 ?01.64 183.75

IT53 1381.0 1362.2 1265.6 1206.4 1139.1pe 17,169 16.951 18.,268 15.709 15.415

TB 470.5 1451.7 1374.8 1310.5 1241.4

Page 25: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*t F34/T7 STUDY Alt*I ESTIMATED PERFORMANCE LYNN MlASS, APRIL 26, 1979

ICASE 59.0000 60.0000 61.0000 61.0000 63*0000

ALT 0. 0. 0.: 0. 0.X?4 0.6000 0.6000 0.6000o 006000 0,6000ERAMt 1.0000 1.0000 1.0000 1.0000 3.0000W839 0. 0. 0. 0 0.

IPANS 14.696 149696 14'.696 14.696 1;.696TAMS 518.67 518.67 518. 67 518.67 518.67P2 18.749 386749 16,:749 18.749 16.749T2 556.13 556.13 556. 13 556.13 556.13

__ PMSD 9569,3 893S,8 7005A6 4657.5 3261.5S__- EPWSD 10153.9 9404.4 7092.0 4703.7 2969.3*SFC 0.3986 0*4010 0,41S3 0.4463 0.4899IESFC 063759 0*3810 0.4102 0,4609 0.5381

WFT 386.04 3583,-3 090 2166.0 3597'6N383079 307.62 56.70 .100099 .191.52wl52,434 50.691 43.;646 36.989 31,556

X14L 11768. 11416, 9882. 8442, 7437.P33 326.43 312,62 Mo8Sb 209.,8 170.94V83 1389.9 1372.5 1296,5 1220.7 1152.1

pe170t 170090 16.356 15.834 15,478

TO16,142--36. 301 24

Page 26: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I *e T734/T7 STUDY At 0

I ESTIMATED PgRPIIRMAP4CE LYNN MASS. APRIL 26v 1979

CASE 6490000 050000 bb00000 67o0000 65.000

5'ALT 0. 0. 0. 0. 0.* m 0.7000 0.7000 0.,7000 0.7000 007000

ERAHI 1.00000 1.0000, 160000 100000 1.0000W539 0. 0. 0. 0. 0.IPAMB 14. 696 14.696 1;,696 14.606 14.696TAM$ 518.67 S18.67 5186? 518.67 518.67p2 200390 20.390 200390 200390 20.390TZ 569.65 569.65 569w65 569.65 569.65PWSD 10150.1 9520.4 7469.2 5225.3 3541sEPW3D 10603.S 9845.6b 7356.1 4641.1 3014.2SVC 0.3811 0.3885 0.4016 004287 0.4659ESFC 0.3706 0.3756 0.4077 00462? 0.5475WFT 3929.e4 3696.3 2999,3 2239.9 1650.2FN 255.15 182.97 w63.* 66 -21b.24 .296.95wl 54.;421 52.767 4S.424 38.667 33*09kENI. 115441 11226. 96690 6331, 73660P83 338.81 325.40 269'11 21l9.41 179.26T53 1401.8 1364.7 1306.6 1234.4 1166.6P8 17"466 17.274 16,487 15,918 15,544TO 14S4,.0 1432.1 1356.1 1290.8 12200?

WN-

Page 27: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

!I** TF34/T7 STUDY Al **

EsTIMATFD PERFDRMANCE LYNN HASS. APRIL 26# 1979

CASE 69.0000 70.0000 710 0000 72.0000 73.0000

U ALT O. 0. 0. 0. 0.XM 0.7500 0.7500 0.7500 0,7500 0,7500ERAMI 1,0000 1.0000 1.0000 1.0000 1.0000WB3Q 0. 0. 0.' 0. 0.PAmB 1L6b9b 1406 9 6 14,696 14.69b 14.696TAmB 518.67 518.67 518.67 518.67 518,67P2 21.349 21,349 21,349 21*349 21,349T2 577.19 577.19 577.1 577.19 577.19PWsD 10194.2 9849,4 7729:7 S433:3 3700:0iEPwSD 10495.2 10077.1 7496,8 49t5,2 3029,5

SFC 0.3814 0,3820 0.3qq6 0,4198 0,4539ESFC 0.3705 0.3734 0 4069 0,4 4 0,5543WFT 3888,1 3762.8 3050.3 2280.7 1679,2J FN 158,12 119,57 -122.30 -272.11 -352.16Wl 54.853 53.943 46,451 39.37 33,958XNL 11294. 11125. Q575, 8285, 7357,

* P8 3 340.00 332,b5 275.21 22*.92 183.95TB 3 1400.7 1391.4 131S.9 1242.2 1175.0P8 17.499 17.381 16.577 1s.985 15.585T8 1438.4 t14,b7 135193 1285,5 1215.1

SI!I.

I

Page 28: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I -

I ** TF34/T7 STUDY Al **ESTIMATED PERFORMANCE LYNN MASS, APRIL 2bp 1qq

CASE 740000 75.0000 76,:0000 77.0000 78,0000

ALT 0. 0. O. O 0.XM 0.8000 0.8000 0.8000 0.8000 0,8000

- ERAMt 100000 1.0000 11*0000 1.0000 190000WB30 O 0. 0.' O. 0oPAMB 14.696 140696 14.696 10.b9b 14,696TAMB 518.67 518,67 518.b7 518.67 518,67P2 22.40q 22,409 22.409 22,409 22.40972 585,20 B85.24 585.24 585.20 585.24PWSD 10181.7 10181.5 8014.9 5b59,3 3872.t

f EPjSD 10291.5 102 9 i.b 7b29,9 098s.b 3039.7SFC 0.3760 0.3760 0.3873 0,4107 0.4417ESFC 0.3719 0.3719 0.40bB 0.4b62 0.5627WFT 3827.8 3827.8 3104.2 2324.0 1710.5FN 54.07 54.20 -189.59 -331.75 -409.87wt 55,151 55,1st 47,550 40,b6b 34,895XNL 11011. 11011. 9472. 8245. 732b.PB3 340.00 340000 281.73 230.89 189,04TB 3 1398.t 1398.1 1323.5 1250.5 1183.7P8 17.495 17.496 16.647 t6.053 15.630TO 1421.0 1421'0 1346.0 t280,0 1209.3

I, I

/I

11I

Page 29: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

ITF34/T7 STUDY Al **

ESTIMATED PERFORMANCE LYNN MASS. APRIL 2o T979

CASE 10.0000 8110000 82.0000 83.0000 84.0000

ALT 5000*0 500000 50000 5000.0 500000". . .02000 0.2000 0;2000 0.2000 0.2000ERAMI 160000 1.0000 1,0000 t.0000 1.0000WB3Q 00 0, 0 0. 0.PAM8 12.228 12.228 12w228 12.228 12.228TAMB 500.80 500.84 500.84 500,84 500.54

Pa 12.570 12o574 12.574 12,574 12,574. T2 504.86 504,86 504.86 S00.S4 504.86

PWSD 7889'8 722604 5391,4 3735.1 2435.9EPW3S 8361.4 7b42.'b 5b45.5 3888.1 2522.9SFC 0,4170 0.0227 0.4482 004824 0,5415ESFC 0*3935 0.3997 0,4280 0.0634 0,5228WFT 3290.0 3054.4 2416.6 1801.8 1319 0FN 905.19 834.22 509.28 306.78 174.33Ml 444'243 42.108 35.041 29,071 24,750XNL 11827. 11827. 107000 9020. 7698.P53 27547 259,69 207.61 167o22 134.09T83 1357,.5 133402 1250.9 1172.0 1101.2Ps 14.455 14.217 13.529 13.101 120816To 1459.4 1444.6 1377.8 1310.3 1243.0

ji I .-.

'I_

* [ I ... .

I--

', I* -

Page 30: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TPILIT7 STUDY LI aESTIM4ATED PERFOR'4AMCE LYNN M4ASS, APRIL Zb, tQT9

CASE 65.9000 86.0000 87.0000 88.,0000 $9,0000

ALT 5000.0o 5000.0 50000 5000.0 500090X14 0.3000 003000 0;3000 003000 0.3000ERAMI 1.0000 1,0000 1.0000 100000 1.0000WB30 0. 0. 0. 0, 0.PAMB 12-.228 12*228 12.228 12.228 t2.228TIMS 500.84 500,84 500.84 S00.64 S00,964

__P2 13016 t3.016 13.016 13.916 13001612 509.89 309.89 509*69 5o9V69 509.89PwSO 8065i? 7375.4 S555.1 3857.? Z536,6

__ EPWSO 62.S 7908,6 5861.6 4020.8 2609'5-~sFC 0.9123 0.4181 00.441t 0,473? 0.5285

ESFC 0.3831 0,3899 0.4151 0,454S 0.5136WPT 3326o,7 308319 2450,6 1821.3 1340.8FN 820.181 712.54 409.19 217.93 97.17ws 446840 42.621 35.665 30.02? Z5.304

1XNL 118270 11127, 10637. 8969. 769* P53 279.18 262.85 211.11t t70,36 13708

153 1361.1t 1338.0 1255,9 1117.3 110791aPB 1401O9 14.263 13.57? t1o.12 120832

To1 1456.2 141.S 1372.8 1305.6 1231'5

11 -T

Page 31: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

T-1

,, TF34/T7 STUDY Al **ESTIMATED PERFLRMANCE LYNN MASS. APRIL 26o 1979

CASE 9000000 91.0000 92,0000 93.0000 9400000

ALT 5000'.0 5000.0 500000 5000.0 500000, . . . 0.4000 0.4000 0.4000 0.4000 0.4000IERAII 1.0000 1.0000 1:0000 100000 100000

WB3Q 0. 0. 0. 0, 0.PAMB 12,228 12.228 12.228 120228 12,226YAMS 500.84 500.84 500.84 500.84 500684

I P2 13.654 13,654 13.654 13.654 13.654..... T2 516.93 516093 516,93 516,93 516.93

PWSD 8280,3 7588.9 57868 4028.8 2674.7EPWSO 8972,8 8182.6 b097,8 415863 2695,?SFC 0.4065 0.4119 0.4317 0,4623 0.5123ESFC 003751 0.3820 0.4096 0,4479 005083WVT 3365.6 3126.1 2497,9 186205 1370.2FM 693e99 595.01 311,58 129.82 21003WI 45,478 43.358 36.538 30.79? 26.059XNL 11827. 11827. 10548. 8893. 7677,P83 283.16 267,39 216.48 174,75 141.15TB3 136409 1343,3 1262.8 118405 1115.0p- 14.571 140329 13.633 13,164 12,864T 1453.2 1437.8 1366.2 1299.3 1230*5

3

I

I

Page 32: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I** TF34ITT STUDY Al 0*

i.... ESTIATED PERFORMANCE LYNN MASS. APRIL 26p 1979

CASE 95.0000 96.0000 97.0000 98o0000 9900000

ALT SO00.O SO00O O 5000.0 S0000 SO00oO-[ENI 0.5000 0,O000 0.5O000 0,5000 0.5000I CRAMS 1.0000 1.0000 1.0000 1.0900 190090

NB30 0. 0, 0. 0 0.PAMS 12.228 , 12.228 12.,228 12.228 12.228

TAB 500.64 5.0.84 50OWS4 500.84 S00.60Pa 14,507 t4,507 14,S07 14,507 14,SOT

T2 525.96 52S.98 5S.s96 525,90 525.96PW8D 8ShOS 7871.3 6090.;$ 4247,1 2856.9

OPW8D 927346 6469.6 6358.7 4302.6 27848.PC 0.3994 0,4042 0,4203 0,0491 0,4931

0SFC 0,3667 0,3756 0.02S 0,4433 0.5058WFT 34191 3t8l3 2ssS.T 190?5 14006.N 571.91 479.6S 214;80 44.S2 -57.76

Ni 46.375 44,328 37.693 31.600 27.04SXNL 11827w 11627, 10446. 661t 76STP53 28875 273.37 223.32 180.05 146.47T83 1370.6 13O1 1271.S 1194.2 1120.7

- P6 14,656 14,414 13.715 13.231 120906TO 1449.0 1432.7 1357.8 1291.6 122292

LI

* . -

74

Page 33: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

1** TF34/T? STUDY At *

ESTIMATED PERFORMANCE LYNN MASS. APRIL 26, 1979

CASE 100.0000 101.0000 102.0000 103.0000 104.0000

ALT 5000.0 SO000. 500000 S0000O 5000.0XM 046000 0.6000 0.6000 0,6000 0,6000ERAMI 1.0000 1.0000 10000 110000 10000WB3Q 0. O 0. 0, 0PANS 12028 12,228 12,228 12.226 120226TAMB 500s84 500,64 500.84 500.64 500.64Pa 15.600 1S600 15,600 150600 15,600

.. T2 537.04 537.04 537,04 537,04 537.04PW3D 8908.7 8207.97 6458,4 4522.S 3070.5EPWSD 9569.S 67S4.9 6632,0 44490 2862l1-TC 03915 0.3954 0,4074 0.4340 0.4727ESFC 0.3637 0.3707 0.3967 04407 0.5071WFT 3487,3 324S,3 2631,2 1962,7 10S1*a

P 494069 365,S9 116.02 .45.7S5 139.24NI 47wS5 3 45.471 39.054 33,047 26.219XNL 11627 11814. 10261. 6712. 7621.PB3 296.08 280.41 231.38 187.53 152.85T53 1378.6 1356,2 1262.3 1205.6 1137 3

P6 144776 14525 13,616 13,305 120966To 1444.0 1427.0 1348.4 1262.S 1212.5

I

I-

t _

I_.

'!

1

Page 34: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**TF34/77 STUDY Alt*J EST14ATED PERFORMANCE LYNN MASS. APRIL 26s 1979

*CASE 105.0000 106.0000 107.0000 108,0000 109.0000

ALT 10000.0 10000.0 10000.0 10000.0 10000.00EM 0.2000 0.2000 0.2000 0.2000 002000ERAMI 1000 10000 10000 10- 0000 oo 1.0000W83Q 0. 0. 0. 0. 00PAWS 10.106 10.106 10.106 10.106 10.108YAMS 4163.01 483.01 463.01 053.01 483.01P2 10.393 10.393 10,393 10.393 10.393

- T2 468.69 46,69 466,69 486.69 466869PWSD 72966;1 6710.1 4980,3 3487.2 2267.2EPWSD 77580~ 7116.12 5205,0o 3615.6 2371.7SPC 0.4098 0.4134 0.4386 0.-4668 0.5198E$FC 0,3653 0.3898 004182 0,4493 0.5011WFT 2989.5 2774,0 2176,6 1824o6 1186.5

- N 939.98 628.78 499. 42 302075 172.36"1 40.003 38,029 31,,241 26.246 21,969X NL 11827. 11627. 11067. 9393. 7924,P53 249.12 234,59 165.12 146.96 119.19T53 1349.9 1325.6 1237.5 1158.6 1067.1Pe 12.290 12,048 11.347 10.933 10.651TI1439.4 142393 1361.10 1291.6 1224.2

Page 35: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T? srUDY At aEST14ATED PERFOJRMANCE LYNN M4ASS. APRIL 26p 19

ICASE 110.0000 111*0000 112*0000 t1390000 114,0000ALT 10000.0 10000.0 19000.0 10000.0 10000,0

0. 0000 0.3000 00-3000 0*3000 0,3000C RAM4l 1.0000 1.0000 1.0000 10000 1.0000W530 0. 0. 0. 0. 0.

PAI 0006 10.106 10.106b 10.106 10,106IAMB 483.01 083.01 483.01 483.01 483.01P2 100:756 tools$ 10.756 10.756 10075812 491.74 491,74 4916'74 491,74 491.74PW5D 740.9, W8boi 5105.1 3eta1.28374.00EpWSD 8060.6 7307,6 5406,2 3746.1 2452*2SFC 0.40S5 0,4090 0.4320 0.4602 0.5064ESVC 0,3748 0,3796 0.4078 0,4397 0,4922WFT 3021.0 2604.2 za05,,5 1648.1 1107.0F"829.56 723.47 412314 2270,0 10b.35

WI 401106 38.525S 31.;b7 26.7?48 .22.4SSXNL 11827. 11627, 10994. 9334. 7901.P83 252,25 237.64 18B.24 151.79 121.71T83 1353.0 1329.9 1242,3 1164,1 1092"oP8 o 23 38 12.094 11.388 10.960 10,66916 1436,8 1420.5 1356.1 1286.8 11.

Page 36: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/r7 STUDY Alt*

ESTIM4ATED PERFOlRMANCE LYNIN MlASS, APRIL 26p t979

CASE 115.0000 116.0000 117-0000 116,0000 t19,0000

ALIT 10000,0 1000000 10000.00 10000.0 10000.0X40,4000 0.4000 0"6000 0,4000 094000

ERAMI 100000 1*0000 1:0000 1.0000 1.0000W530 00 0. 0. 0. 0.PAMB 10.106b 106106 10.106 10.106 10,106jTAMS 483.01 483,01 483,01 483.01 463.01P2 116286 118286 11.266 11.286 111266TZ498,53 496,S3 498*S3 498wS3 498,53jPWSO 7663,4 7063.6 5309.2 3740.7 2493.3

__EPW3D 8373.5 7615.7 5630.5 3890.0 2534.8SP.C 0,3999 0.4031 0*4230 0.4492 0.4943ESFC 0,3660 0,3710 003969 0,4319 0,4862wPrT 3064,4 2847.4 ?245.9 168062 1232,4FN724.64 624,54 327.,16 152.37 42,32

wl 41.199 39,239 32.10l 27.434 23,102XNL 1162. 1182711 10893. 9243. 1664,F53 256e5 242.04 192.65 155.68 123.21T93 135701 1333,6 1248.9 1171.1 1100.9pe 12. 411t 12.167 119,440 10.999 10.703To 1433.3 1416,7 1349,4 1280.1 1212.1

Page 37: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

aTF34#fTY STUDY At

I EST14ATED PERFORM4ANCE LYNN MASS. APRIL 261. 1979

CASE 120,0000 121,0000 122.0000 123,0000 124,0000ALI 10000.10 10000.0 10000.0 10000.0 10000.00X40*5000 0.5000 0.3000 0,5000 0.5000

ERAMZ 1.0000 1.a 000 1:0000 1.0000 1.0000WONQ 0. 0, 0. 0, 0.

EPWSD 67l0.j2 79621-S 5673.2 4045.1 2621.2

wrr 3122.4 2898,0 2298'5 1722.0 1265.

T03 132,91 1339,4 12S.3 11.0 110.3To 1429A0 1412.2 1341.5 127201 1203.6

Page 38: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/? STUDY Al *

ESTIMATED PERFORMANCE LYNN 4ASS, APRIL 26, 1979

-- CASE 125.0000 126.0000 127.0000 128.0000 12900000

ALT * 10000, o.0 10000.0 10000.000 10000.0xm0.6000 006000 016000 0,6000 0s6000

CRAMS 1.0000 1.0000 1.0000 1,0000 100000W830 0. 0. 0.l 0, 0.P4MB 10,106 10,106 10,106 101,106 10,106TAMB 483.01 483.01 483, 01 483.01 483.01pa 12,;154 12.894 12*.894 12.894 11,69472 5t1.93 S17,93 517493 S17.93 517093

8WD 20,10 7613,3 590i.2 4200.3 2857.7EPW8O 902816 SZ4l.7 6140.6 4201.,3 2720,63FC 0.3653 0,3883 0.4007 0,4219 014578ESFC; 0.35aS 0.3587 0.36st 0,4218 0.4008WFT 3183.0 2956.1 2364,9 t17210 1306.1

-PH 522,22 427,50 164.16 0.,70 -93.18wl 43.126 41.107 34,714 29*434 25,033XNL 11827, 11827, 10bab. 9015. 7792,*P83 26&157 253,56 205,70 167.04 135963783 1369.0 t347,1 1267.5 1190.8 1122.1ps 12*16z0 12.356 11.610 114122 109801

TO 1424.4 1407.4 1332.5 1263.3 119493

Page 39: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T? STUDY At *E3TJl4ATED PERFO)RMANCE LYNN M~ASS, APRIL 2b, t979

CASE 130.0000 131,0000 132,0000 133.0000 134,0000

ALT 10000.0 10000.0 10000.0 10000.0 10000.0M07 0.07000 007000 0.7000 0,7000!RAM:10o00 1 :0000 1 :0000 1 :0000 oo

PAH 10.106 t0.106 10.106 10.106 10106

P214.023 14,023 t4,,023 149023 14,023T2530.54 530,54 530,54 530.54 530.54

ViM 8618.7 79bb.T b2940? 446S,9 309906l7w 9337,6 8532.6 b429,6 4351.5 z811.5

SFC 0,3770 0,3797 0,3882 0,0075 0,4375ESFC 0*31480 0,3545 0,3801 004201 0,4823

WT 3249,6 30214.7 2443,7 182802 1356.0FN 419.19 329.9? 78.66 o78.37 -168.0?w'd 44,248 420322 36,.196 30.712 26497

IXNL 11827. 118279 10470, 8677, 7750,P83 275,53 261,04 214.50 174.31 142.40'153 1376.4 1356,2 1279.6 1203.6 1135.6pe 121-750 12,485 116731 t11.210 10.666y8 1420.0 1402.0 1322.8 1254.'2 1183.8

A7

Page 40: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I** TF34/T? STUDY Al *0

.. ESTIMATED PERFORMANCE LYNN MAS, APRIL 26, 1979

CASE 135,0000 136.0000 137;0000 138,0000 139,0000

ALT 10000.0 10000.0 10000.0 10000.0 10000.0Im 0.750 0.7500 0, TSOO 0,7500 OTso0ERA1 1.0ooo0 1,0000 1.0000 1.0000 1.0000WB3Q O. 0. 0. 0, o.PAMB 1O. Ot 10.106 10106 10.106 10.l0bTAMB 483.01 '83.01 483.01 483.01 483.01P2 14,683 14.683 14.683 14,683 1o,6B83T2 537*57 537,S7 537*5? 537"57 537,S7POD 687.9 8162.2 6511.3 4650.8 3226.9EPWSD 9503,6 8677.8 6576.3 4428.2 284S.9SVC 0.3T6 0,3751 0.3818 0.3999 0,4277

IESC 0,3461 0,3528 0.3780 0.04201 0.4849_lT 3289.6 3061.8 24S5.8 1860.1 1380.1PN 367.72 280.61 35.39 .121.15 w207938vil 44.,941 42.985 37.000 31.438 26,968XNL 11827, 11827. 10361. 8806, 77171P83 279,84 265.12 219.2'6 178044 146.08tB$ 1381. 1361.2 1286.1 1210.7 1143.2

. P8 12.823 12.5S7 11.794 119254 10,903Te 1417.2 1399.2 1317.8 1249.3 1176.6

I-

II . .

I

Il

Page 41: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

.* 734/T7 STUDY Alt*ESTIM4ATED PERFORMANCE LYNNJ MASSO APRIL 26# 1979

CASE 140,0000 141.0000 142.0000 143e0000 144.0000

ALT 10000.0 10000.0 10000.0 10000.0 10000.00AM 01oo 8000 600 0600 0,6000 0.8000ERAMIl 1.0000 1,0000 1:0000 1.0000 1.0000W8d3Q 0. 0. 0. 0. 0.pAma 10.106 10.106 10.1106 10.106 10.106T AMS 483.01 483.01 483.01 483.01 'i83*01P2 15,412 tS,412 £s'12 15.412 15.412T2 545.06 545.08 545.06 545,06 545,05PWSD 9041A~ 8408.7 6745,5 4626.3 3363s,2EPW3D 9665.3 8868,6 6725.0 4504,6 286b0SPC 0.3683 0.0696 0.3751 0,3923 0,4178

fESFC 0,3446 0.3S07 0.3761 0.4205 0,466Wry 31t30,2 3109,9 2530.1 1894.1 1405.3FN 316.22 234,62 -10,47 -165016 *248.59NI 45.653 43s550 37.856 32.221 27.679X- NL 11627. 11725e 10236. 8730, Y679,P53 284.28 270.45 224,33 182.89 149,95

T 83 1386.s 13b7,4 12919 1218.2 1151.1- pe 12.913 12s651 111868 11.304 10.941

To 1414.7 139500 1312.5S 1244e2 1173,4

IA

Page 42: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/T7 STUDY Al **

EST14ATED PERFORMANCE LYNN 4AS8. APRIL 26# 1979

CASE 145,0000 146,0000 147,0000 148,0000 149.0000

ALT 15000.0 1SO00. 15000.0 15000,0 15000,0.. 0.3000 0.3000 0.3000 0.3000 0,3000

F ERAMI tO0000 t.0000 1.0000 t.0000 t0000WB3Q 0. 0. 0. 0. 0.

PAMS 8.294 8o294 8.294 8.294 8,294I TAB 465.18 465.18 '465.18 46516 465.18

! P2 8.829 8.829 8.829 8.829 8.829T2 473,59 473,59 473 59 473.59 473e59

- PWSD 6853.7 b2827 4656.08 3263,4 2209.1- EPWSD 7'46"O 6806.2 49S2,5 34509S 2292.8

SFC 0.3998 0.4026 0.4240 0.4490 0*4902ESFC 0,3673 003717 0.3987 0.4273 0.4723

2F 7q04.4 2529,7 1974,4 147493 1083.0FN 841.09 " 725,70 410,03 231,63 116.04wI 36,580 34.55 28.126 230608 19.860XNL 11827. 11827, 11338, 9685, 81600PB3 227,86 213.20 166.66 134,05 107,72TB3 134b,2 1320.3 1227.9 114903 1078o3

Ps 10.496 10.227 9-504 9,099 8.826. T8 1417.8 1401,'9 1340.1 1269.9 1200.6

I . .

I °

• ,I.I]

!'

Page 43: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/77 STUDY Al *

ESTI41ATED PERFORMANCE LYNN MASS* APRIL. 26 # 1979

MAE 150.0000 151.0000 152.0000 153.0000 1S400000

ALT 15000.0 15000.0 15000.0 15000.0 15000.0XM 0e4000 0*4000 0'4000 094000 0.4000ERAMI 1.0000 1.0000 1.0000 1.0000 140000WB30 00 0. 0. 0. 0.

SPAMB 8,294 8.294 8.294 8.294 8.294I AMB 465.18 465.18 465.18 46S,18 465.16

P2 9. 261 90261 9126t 9026t 9,261- 2 460.13 460.03 480,13 480o,13 480.13

PWSD 710606 6465.0 4835.2 3427.60 1317.1EPWSD 7847,8 7060.6 5161.1 3589.1 237S90SFC 0.3947 0,3972 014160 00.4387 0*4771ESFC 0,3575 0,3627 0,3897 0.4189 0.4655

1WVT 2805.3 2567.9 2011.4 1503o4 s105.bFN770.45 640,0? 338.91 168.52 b0.15wl37,.630 35.175 28.790 24.215 20.420

EX4L 11827. 11827. 11255. g997 8117.P53 234e40 217,03 170.'62 137.48 110074T83 1353,6 1324.5 1234,4 1156,3 1086.0

Ie 10.618 10.293 9w556 9.137 6.653

TO 1412.7 1398.4 1333,9 1263.1 1193.7

Page 44: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/T? STUDY At *

EST14IATED PERFOR4MCE LYNN MASS, APRIL 26# 1979

CASE 155.0000 156,0000 157.0000o 158,0000 15900000

AL.T 15000.0 Isooolo 150010 15000.0 1500000xm 0.55000 000 .500 0,5000 0.5000

*UERAMf1 1.0000 1.0000 1.0000 1.0000 1.0000WB30 0. 0. 0. 0, 0.

aPAMB 6,294 8.294 8.294 8,294 8,294jTAMB 465.16 465,18 465.18 465.1 465.16

P2 9.840 9.640 9.840 90840 9,840TZ 488*54 486.54 48854 486954 48.54Pwso 7262.9 6704.3 5066.3 3610.9 2457.6EPWSD 8056.o5 7376,0 5390.0 3737,4 2460.6SFC 0.3886 0.3905 0.4062 0,4267 0,4616

- SPC 003503 0.3549 0.3818 0,4123 0.4610

FN 660011 558.75s 269.29 105.24 2.68wl 37.869 3S,994 a9.636 25.005 21o144IXNL 11827. 11627. 11123o 946. 6062.,P53 235.88 222.08 17S.63 141.95 114.66T83 1354.0 133091 1242.6 1165.1 1095.7ps P8 1049 109383 9,626 9.167 6,887

T 78 1411.7l 1394.1 1326.3 1255.2 1165.4

Page 45: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34iT7 STUDY Al *ESTIMATED PERFORMANCE LYNN MASS, APRIL 26, 1979

CASE 160~o 6.0000 16ol210000 163.0000 164,0000

ALT 15O000 15000.0 1590000 15000.0 Isooo.0xm046000 006000 006000 0.6000 0.6000EAI 1.,0000 1.0000 1.0000 1*0000 1*0000

W830 0. 00 06i 0. 0.*PAMB 68-294 60294 8,294 80294 6,194YAMB 465.16 465.16 465.'10 465,18 465.16P2 to0.581 10.561 10.561 10.561 10.561T2 498.82 498.62 498,62 496,82 496.82PWSD 7559,6 700216 5349,6 3837.6 2623.5IEPWSD 839003 7695.7 5637.6 3895.6 1542.9SVC 0.3813 0.36i? 0.395P 0.4133 0,4452ESFV 0*34S9 0,3483 0.3750 0.4071 0.4594Wry 2882.3 2680.1 21%4.2 1566.1 1168.1Fm 575.84 480o44 199.51 40.23 N55.92WI 36.624 37.014 30,660 2S,971 2,005XNL 11627. 11827. 10960. 9344. 7963,P53 241.62 226,36 181.74 147,42 119,31T83 1360.0 1336.6 125213 1115.5 1106.6Re 10.763 10.498 911712 9o246 $093STo 1407,3 1389,0 1317.b 1246.3 1176.9

Page 46: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T7 STUDY At *

EST14IATED PERFURMANCE LYNN MASS. APRIL 26# 1979

CASE 165.0000 166.0000 167.0000 166.0000 169.0000

ALT 15000.0 15000.0 15000.0 15000.0 15000.0EM 0.7000

ERAMI 1.0000 1.0000 1.,0000 1,0000 21.0000W53Q 0. 0. 0. 0. 0.PANS 8,294 8,294 -8,294 8.294 8,294YAMS 465.18 465.18 465018 465.18 465.16P2 114506 l1.506 11.508 11.508 11.508T.- 2 510.97 510.97 s1ol;97 510.'? 510.97PW3D 791SO, 7323.5 5b99,8 4109.1 2636.0

_EPWSD 8749-4 7995.3 5918,8 4065.6 2636.0SPC 0.3733 0.3745 0.3631 0,3990 044268ESFC 0,337? 0,3431 0.3689 0.4033 0.4592IWF7 2954,7 2743.0 2183.0 1639.6 1210.5FN 495.72 399,15 130.14 w25.80 -118.82WI 39.i992 38.074 31.950 27.125 23008XNL 11:2?; 118279 107670 9175. 79040

P8 4,9 234090 189.34 153,96 125.14T93 1367.3 1344,4 12b3,7 1167.4 1119.4

jP8 10.910 10.624 9,823 9,329 8.992T8 1402,6 1384.2 1307.6 1236.6 116.9

Page 47: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

IESTIMATED PERFORAC LNMASS APRIL 26, 1979

CASE 170,0000 171.0000 172.0000 173.0000 114,0000

ALT 15oo000 15000.0 15000.0 isooo~o 15000.0EM 0.7500 007500 017500 097500 017500E RAMI 1.0000 100000 1.0000 100000 1.0000W83Q 0. 0, 0. 0. 00PANS 8.294 8,294 6,294 6.294 60294T AMS 465.18 465.16 465.18 465.18 465.16

_ 17 12.049 12o.049 12.049 12.049 12.04912 S17.74 517.74 517,74 917.074 517.74PNSO 8099W4 7497.1 5699,6 4265.4 2959.7EPWSD 6915.6 6142.4 6071.6 '155.7 2686.93PC 0,3691 0.3704 0.3769 0,391S 0,4172ESFC 0.3353 0.3410 003662 0.4018s 0.4596WP'T 29690*7 2777.0 2223.5 1669.9 1234.9FN 452o66 357.57 951,26 @60082 -151.31WI 400569 38.671 32w696 27.795 230709XNL167 11627 iz, 10699. 9106. 7669.P83' 2ob 236,58 193.77 157.76 128.0T83 1371.2 1349.2 1270.1 1194,3 1126.3

10259.26 10692 9,690 90373 9,026

F6O10. 3161-,0 214 169

Page 48: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

* I** TF34/T7 STUDY Al **

.... STIMATED PERFORMANCE LYNN MASS. APRIL 26p 1979

-- CASE 175.0o0 176.0000 177.0000 176.0000 179,0000

SALT S00.O IS000.0 150000 15000.0 O1500.0XM 008000 00000 0-8000 00000 0,8000ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000WB3Q O. C. O. O OPAM8 S.'4 8,294 8.294 8.294 6,294TAM8 465,1C 465.18 46518 465.l18 065.16P2 1?.,647 12,64? IA647 12.647 12,647T2 524.98 524.91 524196 524o98 524.98'*NSD 828b7 766b5 6106.t 4424.8 3096.0EPW3D 9070.2 8296.1 6222.4 4241,4 2745.1

0.SFb O3b 0.3661 0.3709 0.3644 0,407S£SFC 0.3333 0.3392 0.3640 0.4010 0.4598WFT 3023.2 281308 2264.9 1700.8 132623P 407.32 316,94 60s49 *95.34 .163.44wt 41.123 39.322 33.479 28.493 24.414XNL 11827. 11827. 10602. 9019. 7850.P93 256,12 242.59 198.41 161.72 132.29T83 1374.8 13S43 127;.9 1201.6 1133.7PO 11.053 10.770 9.'9*S 9.427 9.o7sT8 1398.2 1379.0 1298.0 122b.S 11S6.1

II1

Page 49: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I** TF34/T7 STUDY At l*

I .... ESTIMATED PERFORMANCE LYNN MASS. APRZL 26v 197

- CASE 10,00000 18100000 18200000 18300000 164.0000

ALT 20000,0 20000.0 20000.0 20000.0 10000.0.. 0.4000.4O00 0.000 .4000 0.4000ERAMI 100000 1.0000 1.0000 1.0000 100000W83Q 0 . 0. 0. 0 0PAMS 6.'53 6,753 6.753 60753 61753TAMS 447.35 447.35 447.,35 447o35 447.351P2 7.541 7.541 7.541 7.541 ?.541T2 461.73 461.73 461,73 46173 461.73PWSD 6214.t 5602.5 4355.3 3099.1 2t24.1EPWSD b866.0 6400,4 4677.0 3265.1 2193,9SFC 003919 003933 0.4101 004302 0,4628KSFC 0.3537 003565 0.3819 0,4063 0.4481WFT 2435.4 22610.9 1756.3 1333,3 93*00

FN 71237 633.89 341;12 175,99 73.96wl 320.256 31019 250237 21.182 17.6651. XNL 11827. 11627. 11530. 9699,. 8358P53 200.91 191.3S 149.65 120,37 97,09783 13340.0 131209 1218.6 1140.9 1070,3Pe 8.847 8.655 7,937 7o534 70275TO 1403,A 1383,7 1319.6 1247.6 1176.6

I

I

i Ii

o . + _--

Page 50: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I** TF34/T7 STUDY Al

ESTIMATED PERFORMANCE LYNN MASS. APRIL 2be 1979

CASE 185.0000 186.0000 187T0000 188.0000 189.0000

ALT 20000.0 20000.0 20000,0 20000,0 20000.00x.000 0.5000 0.500 0M5000 0o5000

FRAMt 1.0000 t.0000 1.0000 1.0000 1.0000WB3Q 0. 0. 0. 0. 0.S.... PAMS 6,1?53 6.753 6,S3 6.753 6'753

TAMS 447,3S 447,35 4473S 447w35 447035Sj,013 81013 j013 j013 ;j0j3

... T2 469,62 469.82 469'82 46902 469o82PWS0 6927,? 6053.4 456;.0 327Z.4 2248,SEPW$O 7316,4 6731'S 4901,2 3419*0 2280,7

SFC 003856 0.3867 0-4006 0,418S 0,49[SFC 0,344t 0,3477 003732 0.4005 0.4426IFT 2S17.3 2340,5 1829.4 J369.4 1009.4FN 669.07 575.23 264,29 124,37 27.26Vi 33.537 31.951 26.003 21.911 tasselXNL 11827. 11827. 11426. 9826 8302,P53 208.93 197,18 154.17 124.49 100.32T63 1343.1 1319.b 1226.5 1149.4 107906Pe 9.010 88764 6;004 79S83 7,312TB 1397.3 137S, 1311.9 1239.3 1168.7

.r !

I,.' .1 I

Page 51: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**TF34IT STUDY Al *

I ESTIMATED PFRFiRMANCE LYNN MASS, APRIL 26p 1979

CASE 190.0000 191.0000 192.0000 193,0000 194,0000

ALI 20000.0 20000.0 20000.0 20000.0 20000.0I i E 0.6000 0.6000 016000 00b000 0,6000ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000

o'83 0. 0 0. 0. 0.

PAMB 601753 6.753 6,753 6.7S3 W.73T AMS 447,3. 735 447.35 447,35 473

P28.616 8.616 8.616 69616 8616T2 479.70 479.70 479.70 479w7O 479.70PW'SD 681';.S 631001 4815.9 3477.4 2406*9EPWSD ?67.36 7032.2 5138,3 3579.0 237400SPC 0.3788 093796 0.390S 0.4056 0,4328ESFC 0.3364 0.3406 0:3660 0.3941 0,4388WFT 2581.1 2395.1 1880.6 1410.5 1041.7FN 607.28 510.44 227.87 71,85 -23.25

wt34.532 32,838 -76,929 220761 19.315XNL 11827, 11827, 11295, 9690, 8234o

Q* 9142 8,872 8.087 lob4S 7,350

TO19, 339 10, 201iIs

Page 52: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

* TF34/ STUDY At **ESTZMATED PERF(RMANCE LYNN ,ASS. APRIL 26, 1979

t CASE 195,0000 196,000o 197.0000 195,0000 199.0000

ALT 20000.0 20000o.0 20000.0 20000.0 2000000I X4 01.7000 007000 1.0000 007000 100000

I XAM 1,0000 100000 10000 00O000 1.0000

W83Q 01 0. 0. 0. 0*PAMB 6.753 6e753 6.753 68753 6,753

I TAMB 447.35 447.35 447.3S 447.35 447.35

P2 9.371 9.371 91371 9.371 9.371T2 49 138 491,38 491.35 491.38 491038PWSD 713?,9 6615.8 5111.5 3716,4 25876EPWSD 803113 7356.2 5394,5 3745.3 24663

.... SFC 0./14 0.3718 0.3796 0,3923 0.4164ESFC, 0.399 0.3344 0.3597 0,3893 0.4370WFT 2649.0 2459.S 1940.4 146,1 1077,?FN 543,73 448,57 171.49 17.S0 -73.64wI 35,607 33.891 28.031 23.767 20.222KNL 11S27. 11827. 11115. 9523, 8138.P83 ?21,84 209.13 166.14 134,99 109071783 135b,8 1333.4 1247.3 117103 1103.4Pe 9.,288 9.009 8.190 70719 7,0409O 7 13883 1369.0 1294.5 122095 1t49.S

S1*

i.

I

I .... .,- - -, .. .. ..J ., . ...

Page 53: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY At **

EST14ATED PERFORMANCE LYNN MASS. APRIL 2o lq79

CASE 200.0000 201.0000 202.0000 203.0000 2040000

ALT 20000.0 20O00.0 20000.0 20000.0 20000.0* xM 0.7500 0.7500 0.7500 O,7S0 O7SO0

ERAHI 1*0000 100000 1.0000 1,0000 1.0000! 83Q o. O. O 0, 0,-AMB 6.?53 767S3 6,753 6,753 b.7S3

TAMB 447.35 447.35 447.3S 447,35 447.35P2 9'.811 9,81t 9.811 9,811 9.811T2 497,90 497.90 497,90 497,90PWSD 7314,2 09314 5278.9 3850.0 2686,0EPWSD 8223,4 7533,4 5532,2 3830.7 2506.5

.. SFC 0,3675 0.3675 0,3740 0,3856 0,0060I ESFC 0.3269 0.3314 0,3568 0,3876 0,4376

WFT 2688.0 2496.9 197t. 1484,7 109608FN 514,11 416.50 143,22 -10.88 .102,bbwi 36.230 340505 28,651 24.334 20*712XNL 11827, 11827, 11014, 9Q30, 8078,P53 225,7? 212093 169.80 138,19 112.36T3 136019 1337.7 1253,4 1177o7 1110.0P8 9.377 9,088 8.250 7.760 7.432TS 1386,0 1366,3 1290.1 1215.8 1144.?

I

. 114,I

'Il,

Page 54: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/Tl STUDY Al **

EST144TED PERFORMANCE LYNN MASS. APRIL 2ot tq7q

CASE 205,0000 206.0000 207.0000 206,0000 209,0000

ALT 20000.0 20000,0 20000,0 20000.0 20000.0am 0.8000 0.8000 0.6000 0*O0;0 0.8000

ERAMI 1.0000 100000 1.0000 1.0900 1.0000W83 0 O. O. 0, 0,OAMB 6,753 6,73 6.753 6.T73 6.753TAMB 447o35 447,35 447.3S 447.3S 447.3SP2 10.299 10,299 10.,299 10,299 10,299T2 504.86 504.56 504,86 504,86 504.86PWSD 7so8O0 6983.8 54b0.3 3991.9 2799,7EPWSD 8421.3 7718.2 5676,b 3917,3 2552,6SFC 0,3635 0,3633 0*3682 0.3789 03996ESFC 0,3241 0.3257 0:.3S41 0.3861 0.4382WFT 272901 2537,0 2010,3 1512.6 11187FN 484.Z1 389.38 114.64 m39.54 -130.99

w! 36.886 35s169 29.323 24.93S 21.2661 XNL 11827. 118Z7, 10910, 9326, 8024.

PB3 229,50 217.03 1,73.77 14t.58 115,36T83 1365,2 1342.4 1260.1 1184.3 1117.0P8 9,472 9.17 8316 7,807 7,465

TO 1383.8 1363,5 1285.2 t21191 1139.8

I..

11

II..

I

Page 55: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

IE T TF34/T7 STUDY Al

ESTIMATED PERrORMANCE LYNN MASS. APRIL 2op 197,'

CASE 210,0000 211,0000 212.0000 213,0000 214.0000

ALT 25000.0 25000.0 2S000,0 25000.0 25000.0X4 0.4000 0,4000 0.4000 0.000 0*4000ERAMI t.0000 t t.0000 1.0000 100000WB3Q o0 0. 0. 0. 0.PAMS 51454 5,454 s454 5,454 5.454

I TAMB 429.5? 42TI52 429.52 429.52 429.52P2 6.090 6.090 6o090 60090 6.090T2 44*,32 443,32 443,32 44332 443.32P4s3 S356,5 5114,6 3838.3 2766.7 1917.1EPWSD S95313 567b. 4141,8 2931.1 1993,1SFC 0.3904 0.3910 0.403 0,4226 0.4508ESFC 0.3513 0.3523 0,3765 0.3989 0.4336WFT 2091.1 1999.8 1559.S 1169.1 864,2FN 64,,89 607.05 328,37 177.89 82.28wi 27,314 26s905 21,.721 18316 15,476XNL 118?, 11827. 11716. 10129, 8585,P53 170.21 16b.08 128.94 104.21 84o13TB3 1313,3 1298,4 1201.3 1124.9 1o53.04Ps 7,309 7,218 6,532 6,169 5,931T8 1396.9 1372,3 1308,0 1232*6 1161.0

Ii

I-.

., II

fI

Page 56: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*;* TV34/T7 STUDY Al **LSTIMA1ED PERFLRMANE LYNN MASS* APRIL 2bp 1979

* " .ASE 215.ooo 216,0000 217.0000 218.0000 219,0000

ALT 250o0. ',u.o 25000,0 25000.0 n. 000.0xEN 0.500( 0.50s0 0;5000 0,5000 0.5000ERA 11000C, 1.0000 1,0000 1,0000 .. 0000

ESFC 0.43 0.3: 0,31 0.47

TATB 429,132 S' 2 290.52 129.S2 02q,52b1 t 50,..310 26.8 0 65.8 6.470013 1,09 413.0 9 4109 1st.9 10.09

78 139 06 318, 100.3 2912.6 2029.0SPW SD 0 7 " T " S-6 2 4 " 371 .

S 3069,S 2080,1

E$FC; 0.o1 0.14 , 33 0:3 613 0,3911t 0.4270IFT ?1 3. 047,7 160S,S 1200*S 888,2

F4N bi5,s S53,90 286 76 13586 44,38Wt 28.cl, R1.6 ;7 61 22,500 169932. 16,03sXNL 11827* 11827, IJ645o 10045. 8522oP13 1 '17,? ' 5 70.73 133,S4l 107.b9 87 14T!33 1322 .4 1304,3 1209,S 1132.9) 1062,4P8 7,460 7.316 61.606 6214 5.9 07To 1.390,6 1361.8 1300.2 1225,! 1. 53.0

I

.1

* I*I

I

Page 57: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I** TF34/T7 STUDY Al **

ESTI4ATED PERFORMANCE LYNN MASS, APRIL 26p 1979

I CASE 220.0000 221,0000 222.0000 223.0000 224.0000

ALT 25000.0 25000,0 25000.0 25000.0 25000.0x| 016O00 016000 016000 0,6000 0.6000ERAMI 1,0000 100000 1.0000 1,0000 190000439 0. 0 0. 0 0.

TAMB 429.52 429,52 429.52 429.52 4?9.52P2 6°58 6 .958 6.958 6,9SS 6.956T2 46e'158 460.S8 460.58 060.56 460SSPWSo 5S.l 5576,5 4277.6 3096.2 2170.7EPWSD 67!5.6 6291.4 46lS.12 3226,4 2175.9SFC 0,1?30 0.3780 0.3876 0,4004 0,4229ESFC 0,33Z1 0.3331 0.3590 0.3842 0.4219FT 22536 21082 7bT.9 1239.6 918.0

FN 59411t 515,75 25171 93,96 3.75NI 29.SS3 28.62! 23.409 19.707 16.741XNL 118r7, 118271 li54. 9950, 8451.P83 J95,95 17b.b4 138.89 112.07 9O,5T83 1333,5 1311.7 1219.2 1142,7 1073.SPs 7,659 7.443 6.695 60272 6,005TO 1383,b 1362.5 1291.6 1216.3 1143.0

I

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Page 58: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF3q/T7 STUDY At **

ESTIMATED OERFORMANCE LYNN MA$3, APRIL 26# 1979

CASE 225.0000 226.0000 227,0000 228.0000 229.0000

ALT 25000.0 25000.0 25000,0 25000.0 25000.0XM 0.7000 0.7000 0.7000 017000 0.7000ERAMI 1.0000 to000 1.0000 1.0000 10000WB3Q 0. 0. O. 0. 0.

PAMB 5,4 34 5,S4 5.454 5.454 5.454g TAMB 429.52 429.S2 429.52 429.S2 42.5ZP2 7.567 7.567 7.S6? 7.5*? 7.56?T2 471.80 471.80 471;80 471.80 47160g PWSD 6354.9 SA968 4547.8 3316.6 2335.3EPWSD 7291.7 6673.s 4876.1 3400.0 2272.2SFC 0.3712 0.3705 0;3771 0.3876 0.4075ESFC 0.3235 0.3273 0.3517 0.3781 0.4168

I WFT 2358.7 2184,7 1714.9 1285b 9st.6FN 579.25 8O.46 203.03 51.61 -39.01wt 31.489 29,.855 24.416 20.635 170557XNL 11827. 11827, 11416. 9840. 6363.P83 196.18 180.24 144.81 117.31 95.35T83 1346.2 1321.3 1230.1 1154.2 1086.0ps 7.9D7 7.b14 6.798 6*346 6.052

I T5 1376.6 1356.3 1282.6 1206.6 1133.4

II

S I'II

II

I

I

Page 59: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**TF34/T? 3TUDY ki *j ~ESTIkTU'~, PERFORMANCE LYN4N MASS* APRIL 26 1979

FCASE 230,0000 231,0000 232,0000 233,0000 23'4.0000

ALT 25O0000 25O00.0 25000,0o 25000.0 25O000030.7500 0,7500 007500 0.7500 0.7500

UtRAMI 100000 1.0000 1.0000 1,0000 1.0000o63 Do 0. 0 0,

PAMS 5 5 ,454 S,454 5,454 5,4S4I-TAMS 42qS5? 429,S52 429-S2 429.S2 429.52P2 7,43 ,237T.923 7.923 7.923T2 478~,05 073.05 475.05 478.05 476.05jWS 60j~ e49.8 'J69b's 3416,6 2425.3fPW3D S 6841.3 5010.7 3490,3 320.9SFC 6.326,72 0.3b66 0.371? 0,3810 0.3996ESfC 0 " 3Z03 0.3242 0.3484 0,3754 0a4178W FT 2217,7 174S.9 1310.3 9b907F4 55.1 456.19 1811,16 20*72 -b0e2?wi 31 938 30.347 24.973 2i113 160003I.XNL 1182?. 11827, 11337. 9757. 6310,P53 1"~.30 t87.58 148,10 120.18 97.76783 A114ylo t3S5.6 1236.0 1160.4 1092.?ps 7.97t 11,1688 6,854 61387 6,084re 1374.7 1353.8 1276.1 1201.5 112S96

Page 60: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** F344/T? STUDY AtESTIMATFD PERFORMANCE LYNN MASS. APRIL Z6, 1979

CASE Z3S°0000 236.0000 237.0000 238,0000 239,0000

ALT 25000.0 25000.0 25000.0 25000.0 25000,0

xM 046000, 06000 0,6000 00.000 0.6000ERAMt 110000 140000 1.0000 1,0000 1.0600W83Q 0 0. 0. 0. 0.PAM35 5...54 59454 S,5 S,454 S,454TAMS 142905a 429.52 429.52 49,52 429,52P2 8.316 8.316 3,31b 8,316 8.316T2 464,74 484.74 484.74 484,74 464,74PWSD 660.5 6205.9 4849,5 3568,9 252402EPWSD 7 64 !.D 7006.b 5143.0 3582.0 2370,6SFC 013636 0.3627 0.3bb4 0,3744 0.3919ESFC 01j373 0.3212 0,3455 0.3730 0.4t73Wr 2 ,0 2250,7 1777.1 133bl 969,3N 28.38 433,22 tS$7; ?.10 -62.96S32.513 30.937 2g.542 21,681 18,491

XNL 1187. t1627. 11235, 9662. 8255.P83 20Z.57 190.91 151.46 123.22 100.40TB3 13,512 1329.7 1242,3 1167.1 1099,9Ps 8,067 7,770 6.915 b.432 6,115T8 1373.0 1351.7 1273.? 1196,4 1123,5

r -

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Page 61: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/T7 STUDY A1 **

EST14ATED PERFORMANCE LYNN MASS. APRIL 20# 1979

CASE 240.0000 241.0000 242.0000 243,0000 244.0000

ALT 30000,0 30000.0 30000.0 30000.0 30000.0X' 0.4000 0,4000 0s4000 0,000 0.4000ERAMI 1.0000 1,0000 1.0000 1,0000 1.0000W830 0. 0. O. 0. 0..PAM ,364 49'364 a.364 4.364 4,364TAMS 411.68 411.68 411.o 411.68 411.68P2 4,873 4.873 4.873 4.873 4.873T2 424.91 424.91 424,91 424.91 424.91PWq1D 4375,9 4375.? 3328,6 2437, 1705.0EPq 4P73.6 4873.3 3606.8 2596.1 1783.7SFC 0.3901 0.3901 0.4033 0,4164 0.4410E$FC 0.3503 0.3503 0,3722 0,3910 0,4219

. wFT 1707.2 t707.1 1342,5 1015.0 752.6FN 550.16 550.04 307w23 175.08 87.00WI 22.712 22,712 18,430 15,664 13,258

I XNL 11780. 11780, 11780. 10329. 8832eP83 140021 140.21 109.58 89.26 72.18TS3 1278.0 1278.0 1183.3 1106.9 1036.1

1 P8 s.-9,2 5.929 5.330 5.014 40798T T8 1361.? 1361.7 1297.5 1219.9 1146,9

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Page 62: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/T7 STUDY Al t*EST14ATED PERFORMANCE LYNN MA88. APRIL Zbo 1979

CASE 245,0000 246.0000 27,0000 248,0000 249,0000

ALT 30000.0 30000,0 30000,0 30000.0 30000.0K i X1 0.5000 0,5000 0.5000 0,5000 0,5O00ERAMI 1.0000 1.0000 1.0000 1.0000 160000

WB31 0 0. 0. 0, 0.PAMB 4.364 4o.36 4.364 4,364 4.364TAMB 411.b8 411.68 011.66 011.68 411.68P 5.178 5.178 5.178 5,178

1-2 432,35 432.35 43213S 432w3S 43253547090 462b,4 3497,3 25b6.6 180S.35pwsr $326A4 5231.0 3808.8 2727.0 1866,0

SFC 0.3843 0.3845 0,3956 004066 0,4288LsFC 0.3398 0.3401 0.3632 0.3827 0.4144WFT 1809.8 177818 1383,4 1043,S 774,1N 5,93 534.67 275,49 141.73 55.47

S1 23.816 23.747 19.103 16.209 13.744XNL 11827. 11827. 11799, 10255, 8762oP83 147.79 146b.6S 113.S0 92.32 74.60

I T83 12908 1288,7 1191,1 1115.1 1044.7P8 6.102 6,077 5.397 5,056 4,827TB 1370.5 1358*'5 1290.7 1212.1 1138,6

III

I

I

II

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Page 63: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY At *ESTIMATED PERFORMANCE LYNN MASS, APRIL 2 6 # 1979

CASE 250,0000 ?51.0000 252.0000 253,0000 254,0000

ALT 30000.0 30000.0 30000.0 30000.0 30000.0XM 0.6000 0,6000 0.6000 006000 0,6000ERAkll 1.0000 t.0000 1,0000 t0000 1,0000

0a3u . 0, O. 0, 0,PAMB 4.354 4,364 4,364 4,364 4.3b4TAMB 411,68 411,68 411,168 411,68 41t,68

P2 56b8 5,5be 5.566 556 5568

T2 '41145 441.4S 44105 441545 441,45PWSD 5081wo 4840.6 3713.1 2722.2 1927.5EPWSD 5822,b 5520,S 4046,9 2669.1 1956,3SFC 0.3783 0,3780 0.3860 0,3957 0,4149ESFC 0.330! 0.3315 0.3542 0.3754 0,4084WFT 192210 1829'6 1433.4 107.? 799'7FN 546,5 501.03 246.01 108.21 22,70w 25.066 24.550 19.936 16.662 14,331XNL 11827o 118271 11711. 10152, 8665.PB3 156,24 151.64 118.45 96.04 77.9?T83 1311.7 1295.6 1200.7 1124.8 1054,8PS 6,312 6.191 5.484 5108 4,862TS 1378.6 1353,7 1282.0 1203.5 1129,4

SI

I,

*1

I.

Page 64: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY Al **ESTIMATED PERFMRMANCE LYNN MASS. APRIL 2b, 1979

CASE 255.0000 256.0000 257.0000 2S.0000 259.0000

ALT 30000,0 30000,0 30000,0 30000.0 30000,0EM 0,7000 0.7000 0.7000 0.7000 0.7000ERAMt 1000 .0000 1.0000 1 .0000 oo 1.0000W80 01 O. 00 0, 0'PANS 4,364 4,3 4 4.364 64 43b4

TAMB 411.68 411,68 411i66 411.68 411.66P2 6.055 6.055 .OSS 6,055 6,05T2 452,20 452.20 452.20 052.20 452.20PWSD 5416.b S096,4 3973,3 2913.3 2069.0EPWSD b274.6 5848,6 4319.4 3032.1 205405SFC 0.3120 0.3711 0.3756 0,3836 0.4009ES7C 0.3211 0.3235 0.3457 0.3667 0.4036

0FT 2014.9 t892,2 1493.3 1118.1 529'5... 5 97 473.68 Z16Sb3 75.06 -9.14

Wl 26.500 25,541 2094b 17.667 15,026XNL 11627. t1827. 116?10 10043. S553,

" PB3 165019 157.73 12Q.40 l0.s 81.73- T83 1324.3 1304,0 1211'6 1136.2 1066.7

Ps b.S4O 6,343 5.594 5,174 4,913T8 1372.1 1348.9 1272.5 1193.8 1120.1

I.

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Page 65: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF341TT STUDY AS *

ESTIMATED PERFORMANCE LYNN MASS, APRIL 26. 1979

CASE 260.0000 261.0000 262,0000 263,0000 264,0000

ALT 30000,0 30000.0 30000.0 30000.0 30000.0XM 0.7500 0.7500 0.7500 0,7500 0,7500ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000WB3Q 0. 0. 0. 01 0,PAMS 4,364 4.364 4.364 4,364 4o364TAMB 411b,8 411068 '11a.6 411.68 411,68P2 6.340 6340 6340 6e340 6o340T2 450,20 458.?0 458,20 458020 458.20PWSD 5606.1 24S,? 4t14,3 3022.3 2151.6EPWSD 527.9 6028,4 4462o3 312ib 2105.6SPC 0.366Q 0,3674 0.3707 0.3777 0.3934ESFC C.3168 0.3197 0.3418 0,3657 0,4020WFT 200?. 9 t927,5 1525,4 tll4 846,5FN S43ot 461.39 205.'14 58.53 -27.10Ni 270420 b16.098 211.496 18.130 15.427XNL 11827. 116270 11572. 9986. 6501'.P03 170.28 161.16 127.64 103,19 83.89TB3 1331.1 1308.4 1218.0 1142.5 1073,3pO 6,679 6,430 5665) S,214 40938To 1369.0 1346.4 1267.8 1188.8 1114.8

I

S I

I

1I

Page 66: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T7 STUDY At *

I ESTIMATE~D PERFOJRMANCE LYNN MASS* APRIL Zoo 1979

CASE 265,0000 2b6.0000 267.0000 268.0000 269.0000ALT 30000.wO 30000.0 30000.0 30000.0 30000.0X4 0.8000 0.8000 00,S000 096000 0,6000

Etl 1.0000 t'0000 1.0000 1.0000 1.0000!4330Q 0. 0. 0. 0fPAMB 4,464 4.364 4, 364 4,364 4,364

TOR 11*8 41,6 41048 411.,68 411.68P? 6.65r, 6165 .655S 6.655 6,655T2 464.61 464.6t 464*'b1 464.61 464061PNSD 5807.8 54i4, 4 4255.7 3137.6 2239'5EPWSO ,. 797.5 6234.0 498.5S 3213.4 2156.0SFC 0.3658 0,3638 0.63655 0,3716 0.3660ESFC 0,3126 0.3160 0&3383 0,3628 0,40061WFT 2124,6 19b917 1555.6 1165.9 564,4

FN 54095 452,97 189.45 41,95 005,04wt28,204 26,770 22,0;25 16.618 15.859

XNL 11827. 11827. 11493s 9922. 64449P83 175.75 165,26 130.75 105.95 6.22T83 133813 13130, 1224.2 1148.0 1060.5jp8 6*833 b.536 51118 5.1258 4,967

To 1366.2 1343.6 126303 1183.9 11096

I 4--

Page 67: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

.. TF34/T? STUDY At **

ESTIMATED PERFORMANCE LYNN MASS. APRIL 26 1979

CASE 270.0000 271,0000 272,0000 273,0000 274,0000

ALT 35o000 3S000o0 35000.0 3SO00.0 35000.0.M 0.5000 0.5000 0.5000 0,5000 0.S000ERAMI 1.0000 1.0000 1.0000 1,0000 1.0000WB3Q 0. 0. 0. 0 0.PANS 3.458 3458 348 3.458 3.458TAM 393.85 393,85 393.65 393.65 39398SP2 4.103 4.103 4.103 4.103 4.103T2 413.62 413.62 413.62 413w62 413,62PWSD 3740A1 3739.9 2991.7 222607 15?3.5EPWSD 4232.6 0233.0 3273.6 2383.2 1642,7SFC 0,3844 0.3845 0.3924 0,4024 0,4237ESFC 0.3397 0.3397 0.3586 003759 0.40S6WFT 1437o9 1438,'0 1174.0 895.9 b66,6FN 405,38 445.82 254.90 14tS2 62.591 19.354 19,354 15.960 13,699 11.613INL 11622; 11622, 11622, 10417. 89530

P83 Its*?? t,78 95,04 78.18 63.31T83 1252.5 1252.6 1171.0 1095.9 102S,3P5 4.SbS 4.867 4*364 4.077 3,872T 78 1331,4 1331.6 1280.'5 1201.1 1127.4

I

- I'I

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II

A ... . ... ._ __,,._ _ _ _ _

Page 68: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

Ia. TF34/T7 STUDY At a'

EST111ATED PERFURMANCE LYNN MASS* APRIL 2b 1979

I CASE 275.0000 276.0000 277.0000 278,0000 279.0000

ALT 3500.0 350ooo0 35000.0 35000.0 35000.0XM 005000 0.5000 0.6000 0.6000 006000IRAI 1.0000 1.0000 1.0000 1.0000 1.0000)3 O. O. 0. 0. O.

-AM 3.,4S8 3.458 30458 3,458 3,456'IAMB 393.85 393485 393W85 393.65 393.85P2 4.103 4.103 4,412 4,412 4,412T2 413.62 413.62 422.32 422.32 422.32

3740.1 3739,9 31b2o.6 2365.2 1684021PW$D 4232.6 4233,0 3472.3 2519,4 1734.2SC 0.3844 0.3845 003849 0,3917 0.4099

FC 0,3397 0*3397 0.350 0.3677 0,3981WFT 1437.9 1438,0 1217o4 926.5 69004FN 445,38 445.82 23332 116.13 37.73wl 194;354 19,354 lb.bSb 14.273 12143XNL 1122. 11622, 11744. 103290 88s5eP83 118.77 118.78 99.15 81.42 66.18T83 1252.5 1252.6 1179.8 1105.5 1035.8

I Pe 4,865 4,867 4,440 40126 39Q07T8 133104 1331.6 1274.1 t192.0 it17.5

II

t f

, -

Page 69: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

f ** TF3'i/r7 STUDY 41ESTIMATED PERFORMANCE LYNN4 4A53. &PI abo W99

CASE Z8OOoO0 Z31.0000 262,0000 283.0000 264,0000

ALT 35000.0 35000.0 35000,0 35000.0 35O000x14 0.7000 0.7000 00.7000 017000 0,7000

EAI 1:0000 10000 10000 1,0000 1.0000

PAMB 3.45 335,048 .58 148TAMS 393585 3.8S 393,85 393.85 393o85P2 4.9 1419 4.196 4,798 41196T2 '632.60 43?,60 432.60 '32w60 432.60PWSD 45l0 S 4408,.0 3388.8 ?226. igloo?EPMSD SZ69,S 5140,4 3725,2 ?66712 1826.8SFC 0a3736 0.3732 0,3758 0,3809 0,39S9ESFC 0.3198 0.3200 0.3418 0,3608 0,3920

WT 1b85.3 1645.1 1273.4 962,2 716.9FN489.98 473,01 217,124 9S102 11971

wl 22,042 21,953 17.572 14.9S4 12*744XNL. 11271827 .ls? 11728. 10219. 877),P93 137.13 135.73 104.53 a5.25 69,43T83 1298.a 1259.9 1191*3 1116.4 1047.2re 13S9,10 1341,3 1265.1 118360 1107.6

Page 70: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**rF$4/T7 STUDY Al *

ESTIMATED PERFORMANCE LYNN M4SS, APRIL 26F 1979

CASE 265000 286.0000 267.0000 288.0000 269.0000

ALT 35000.0 35000.0 35000.0 35000.0 35000.0xm0.7500 007500 0;l~O 07500 0.75 0700

ERAMI 100000 1.0000 1.0000 110000 110000q80 0. 0. 0. 0. 0.

PAP4B 31Gse 3.458 3.058 3.406 3.456lAMB 393.85 393.65 393,85 393.85 393.85

5a .023 5.023 S,023 5.023 S,023T2 438o33 438,33 43S'33 438.33 436.33PW'SD 4720.8 4558,,7 35i.;.4 2615.2 1882.6EPWSD 5554.7 5348.1 3862.4 2744.8 188000

s 003710 0*3703 0.3-08 0.3753 003S6bE3FC 0.3153 0.3156 0.3375 0.3576 0.3692I FT 1751.6 1687,9 1303.b 951.6 731,7FN502964 475.83 209.,22 78.13 -1.66wl22.7b7 22,031 18,075 15.328 13.08S

X4L 11827. 11827. 11684. 10152. 6712.P53 142o0* 139.89 1071t 87,40 71.27783 1308., 1296,4 1197.7 1122.4 1053.5ps S.493 5e423 4.609 4o221 3,973ITS 1365.9 1338.6 1260.3 1178.3 110WO

Page 71: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

h* TF34/T7 STUDY Al *EST14ATED PERFORMANCE LYNN MASS. APRIL 26v 1979

I CASE 290,0000 291.0000 292.0000 293,0000 294.0000

Ai.,T 35000.0 35000.1 35000.0 35000.0 35000.0X4 0.8000 0.8000 0,8000 0.8000 0,8000f E t 1.0000 1.0000 1.0000 1,0000 1.0000

WFT 3 06~ 105 035. 002. 741

PWB 23.459 3.56 3,458 3 ,0 13.4T4MB 393wSS 393,S5 393,BS 393,65 393*85P2 5.273 5,273 Swi73 5,273 S.273Ta 444047 444.4? 444i4? 444w47 444,47

FWSD 4887.0 4613,S 360. 271108 195040EPWS3 5786.3 S398.1 4007.1 2897,5 1931,9SFC 0,3683 0.3664 0*36S8 013697 0,3614ESFC 0.3110 0,3131 0.3333 0,3S46 0,3866WFT 1799'T 1690.5 1335,S 1002,6 747,2FN 508972 443.$8 201041. 65w3S -tS.38

twt 23,5S09 22.656 1611610 15.737 13,44S

XNL 116274. 118270 |t6309 10064," 86400" P53 146. 68 140.0s 110.W66 89.71 73*22

T 183 1315.8 1295.8 1204.3 1128.7 1060'a* P8 5.629 S,428 4.675 492S9 4.000

To 1363.b 1338,6 1255,4 1173.6 1097.0

* I..

II

.I

Page 72: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY Al **ESTIMATED PERFORMANCE LYNN HASS. APRIL 20 1979

CASE 295.0000 296.0000 297,0000 298,0000 299,0000

ALT 40000,0 40000.'0 40000.0 40000.0 40000.0x.o5000 0000 0.5000 0OSO00 0,5000ERAMI 1.0000 1,0000 1:0000 1,0000 1.0000

5 0, 0. 0, 0PAMB 2.720 2.720 2.720 2.720 2.720TAMS 389,97 389,97 389,97 389.97 369,9?P2 3.227 3.227 3.227 3.227 3.227T2 409,5q 409.54 409w54 409WS4 409.54PWSD 3001.0 3000.6 2264.0 1707.? 11q,99OWSD 3397.9 3397.3 2491,4 1824,6 1250.63FC D03668 0,3868 0.3969 0.4063 0.4334aSFC 0,3416 0,3416 0.3639 0.3822 0.4150W T 1160.7 1160.S 906'5 697.3 s20.0FN 360.6S 360.47 188.48 106,22 46904

S15.263 15,263 12.201 t0556 8,928XNL 11565. 11565. 11436o 10132s 8656,P83 94o43 94.43 7,87 60.43 48,80TB3 1253,3 12533 1158.9 t086.4 1014.2P8 3.848 3,847 3w396 3.190 3.032TO 1347,7 1347.5 1288.3 1207.9 113696

I

II

!i1

II

4'L$1 ". H .. ..

Page 73: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

TF34/T? STUDY AtESTINIATEo PERFORMANCE LYNN MAS3. APRIL 26, 1979

CASE 300.0000 301.0000 302.0000 305.0000 304.0000

ALT 40000 40000.0 40000.0 40000.0 40000.0X" 0.6000 0.6000 006000 0,6000 006000ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000WB30 01 0, 01 0. 0.

- PAMB 2.720 20720 2,720 20720 20720TAMB 389.9? 389.97 38;.197 389.97 389.97P2 3,470 3.470 31470 3,470 3,470T2 418.15 416,15 416.'15 418.15 418.15PWSD 3285.5 1241,9 2439.8 1814.3 1293.6EPWSD 3780,1 3728,2 2670.4 1929,0 1331.03FC 0.3809 0,3809 0.3875 0,3976 0,4182ESPC 0.3311 0.3312 0.3541 013740 0.,406S

WT 1251.5 1234,9 945,5 721.4 541.1FN374.56 368.25 174.'66 86.66 28.23

wt 16,7252 16,215 12.819 116005 9.39SXNL 11666. 1166. 11442, 10051. 6645.P83 101.17 100.58 76.54 62.97 51.34T53 1274.6 1270.0 1169.1 1095,8 1026.5PS 4.017 49002 3.462 3o227 39064To 1358.o4 t348,;9 1278.7 1199,1 1124.7

Page 74: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF341OT7 STUDY AltI ESTIM4ATED PERFORMANCE LYNN bIASS9 APRIL 26o 1979

ICASE 30F5.*000 30690000 307.0000 308,0000 309.0000

*ALT 4000090 40000,0 40000.0 40000.0 40000.00.7000o 007000 0017000 067000 0.7000

ERAMI 1,0000 1.0000 1.00000 100000 1.00004830 0f 0. 0. 0. 0.PAI4S 20720 20720 2.720 2.720 20720TAMS 389.97 389,97 389, 97 389,97 389o97P2 3.1774 3*774 3,774 3,774 3*774T2 428.33 426.33 428.33 426.33 428,.33PWSD 3552.0 3259.2 262;.4 1941.0 1396.6EPWSO 4136.7 3733.7 2869.9 3045.3 1410.3SPC 0s3756 0.3745 0;3777 0.3862 0.4034ESFC 0,322S 0,3269 0.3449 0.3665 0,399S

W 1334,0 1220.15 989.8 749,7 563,4FN 379053 307.97 1611,96 67.68 6.73wl 17.1096 15.-964 13W'533 11.539 91897XNL 11827. 11827. 11391, 9950. e669P83 107.02 99.04 80.76 66.00 54.07T83 1291.6 1264.2 1180.8 1106.7 1038.9P$ 4.177 3,962 3,S44 3,274 39096TO 1371s,4 1351.4 1268.7 118907 1113.7

Page 75: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

I -T

TF34/T7 STUDY At AP I 6p 1 7ESTIMATED PERFORMANCE LYNN MASS. PI 2,17

CASE 310.0000 311.0000 312.0000 313.0000 314.0000

ALT 40000.0 40000,0 40000.0 40000.0 40000.0- M 0.7500 0.7500 041500 007500 0.7,00

ERAMI 1.0000 1.0000 1.0000 1.0000 1.0000WB3Q 0, 0. 0. 0. 00PAMS 210720 2,720 2,720 2,720 2.720T AMS 389.97 389,97 369,97 389,97 389097P2 3,951 3.951 3.o95 3.951 3,9S1TZ 434,01 434,01 434.01 434.01 434.01IPV43D 3653-1 3367.6 2724.3 2012.7 1451.5EPWSD 4272.6 3871.6 2982.4 2108,7 16489SFC 0.3725 0.3710 0.3726 0.3803 0,390?ESPc 0,3184 003227 003404 0.3630 0,3969

W 1360.6 1249.,2 1015.2 765.5 575.1FN375.28 305.35 156.,35 11.641 o1.56

[ NL 11821. 11827, 11380o 9894. 8507P83 109.47 101.75 83.17 67.72 55.51T83 1296.5 1270.0 1187.3 1112.7 1005.1

14,246 4,030 3.592 3,302 3,117UTO 1369.2 1348.1 1263.5 1184.8 1106.8

Page 76: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*0 TF34/T7 STUDY Al *

ESTIMATED PERFORMANCE LYNN 4ASS9 APRIL 26f 1979

[ CASE 320.0000 321.0000 322.0000 323.0000 324,0000

ALT 4S00*0 45000.0 45000.0 450000 45000.0U 0.5000 0'5000 ' 0.000 00 sO"

ERAM 16 .0000 1 :0 0000W830 0. 0. 0. *0 0.PAMS 2.139 2e139 2.139 .139 2.139TAMB 389.97 389.97 389.9? 389,97 369097P2 2.38 20538 2.S38 2.536 2,536T2 409,54 409,54 409J54 409,S4 40954PWSD 1977:0 19770o 1699.7 1242.4 864.3[PWSD 2t9003 2190.3 184S.3 131999 896.5SFC 0.3975 0.3974 004038 0,4208 0.45419SFC 0.3S87 0.3581 0,3719 0.3961 004376-FT 785.7 785? 6863 522.8 3920SFN 193.84 193,84 132.30 70.41 29.27wl 10,154 10.154 9,144 70802 6.609X4L 11565. 11565. 10993. 9605. 6163oP53 62069 62.89 54'76 44.78 36922T83 1211,3 1211.3 1148.3 1073.2 1001.4PS 2.779 2.779 2.626 2469 2.361

1 VS 3373,3 137303 1301.1 1226.4 11s7.9

I-

. I" I

Page 77: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/T7 STUDY AtESTIMIATED PERFORMANCE LYNN 4ASS. APRIL a6e 1979

CASE 325,000 326.0000 327.0000 326.0000 329,0000

#447L 45000.0 45000,0 05000.0 45000.0 45000.0xM006000 0.6000 0.6000 096000 0.6009

ERANII 1.0000 1.0000 1.0000 1.0000 1.0000013 3Q 0. 0. 0. 0. 0.PAM$ 20139 Z.139 2.139 2.139 2.139TAMB 389.9? 389.97 389.9? 389.97 389.97P2 2.729 2.729 2,;729 2.729 2.729T2 416.15 41615t 416;15 416,15 418.15P'WSD 2179,07 2177,3 1620.4 1325.6 930.7EPWSD 2441.:8 2439.7 1981.-4 1400.2 95100

-SFC 0,3884 0.3686 0,3936 0,4090 0,4382ESFC 0,34b8 0.3468 0.3618 0,3872 0,4289WT846.7 846.2 716.8 542.2 407,9FN198.46 196,73 121.92 56.34 15.34

wi 10o.883 10.681 9.633 8.165, 6,946XNL 11666. t1186; 11010. 9542. 8126.

P936791 7,6 5766 46.65 36.06T83 1232.8 1232.6 1160.2 1063o? 1013.3Ps 21876 2,878 2. 676 2.498 2o362

To 7 373,;9 1373,8 1290.2 1216.5 1146.6

Page 78: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

**TF3q4#T? STUDY At *ESTIM4ATED PERFORMANCE LYNN MASS,' APRIL 26p 1979

CASE 315.00060000 31 7joooo 31 3S0000 319.0000

ALT 40000*0 40000.:0 40000.0 40000.0 40000.0X4 040180000 0 *8000 0 18000 0SOO 08000ERAMI 1.0000 1.0000 1.0000 190000 160000W830 0. 0. 0. 0. 0.

TAMS 389.97 389,97 389"'g? 369.97 369.97

£SFC 0.319S 0,318 366 0,3543 0.369

PH374.03 303.60 I136 48.56 w12'14Wl 17.956 160860 14.383 12.169 10.;43XNI. 11827. 11627, 11363o 9635. 8446.P83 112.34 104.5b685078 69.57? 57.03T83 1302.0 1275.7 1194,2 1119.1 l051.7Ps 40330 4.107 3,;647 3.332 3,138

TO' 1367.1 1345.2 1258.3 1179,7 1103.8

Page 79: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/TT STUDY Al **

ESTIMATED PERFORMANCE LYNN MASS. APRIL 26o 1979

CASE 330.0000 331.0000 332.0000 333.0000 334,0000

ALT 45000,0 4S000.0 4Sooo 45000.0 45000,0S XF4 0.7000 0,7000 0.7000 0,7000 0,7000IERAMI 10000 10000 1.0000 1 o0000 10000WB3Q 0. 0. 0s 0. 0.

-pAms 2139 2.139 2.139 2,139 2,139TAMS 389.97 389.97 389.97 389.97 389.97P2 2,;968 2.968 2.968 2,968 2,966T2 42833 428,33 428.W33 42603 426.33PNSD 2e51.5 2343,8 1968.0 1429,5 1010.1EPWSD 2781.4 2644.1 21*2.6 14954 101104SFC 0.3803 0.3806 0.3830 0o3962 0.4216ESFC 0.3352 0.3374 0,3S18 0.3788 0.4211WFT 932,3 892.1 753.7 566,4 42S.9FN 214.16 t94.91 113.32 42.79 Ossw1 110782 11SO6 10.233 8.616 7,345XNL 11827. 11827. 11037. 9497, 8087.-P83 73.88 71.65 61.25 49.43 40.24T83 1259.2 1245o6 117040 1096,4 1026.9Ps 3.018 20965 2.741 2.536 2,408To 1356.4 1369.2 1278.2 1205,1 113493

S41

Ii

I

"I* --

I

Page 80: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

** TF34/T7 STUDY At **ESTIMATED PERFORMANCE LYNN MASSO APRIL 26, 1979

CASE 335.0000 336.0000 337.0000 338.0000 339.0000

ALT 4SO00o0 45000.0 4500. 509 0000o.0X 0.750 007500 0 .7500 *?So 0,7500ERAMI 10 0000 1t0000 10000 140000W53Q 0 0. 0. 0o 0.

. PAMB 2139 2.139 2.139 2.139 2,139TAMB 389.97 389.97 38997 38997 389*97P2 31107 3,t07 3O,107 3.107 3.107T2 434.01 434.01 434.01 434.01 434.01PW8D 25841 2440,0 2047,S 1490.9 OSbbEPw$D 2949,5 2762.0 2227,3 15S0.2 104S5SPC 043?63 0.3763 0.3776 03894 0,4126ESFC 0.3296 0.3324 0,3471 0.3745 0,4t?WPT 972,3 918,1 773,2 580.S 436*1FN 221.34 195.06 10590 35.90 -6.75wt 12.261 11689S 10.5S1 86882 7,S77XNL 11827. 11827. 11032, 9484 Soo,

-P53 77o04 74.05 63,14 50,94 41*SOT83 1210,2 1252,5 1181,0 1103,6 1034a6

- P 3,196 3.020 2.77 2,558 2,423To 1387,S t364,1 1272,S 1198,6 1121,5

I-

SI+

I

~I

++it

* - .-

Page 81: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

*TF34/TI STUDY Al *ESTIMATED PERFOlRMANCE LYNN MASS, APRIL 26. 1979

CASE 340.0000 341,0000 342.0000 343.0000 344,0000

*ALT 4500001 4O00.0 45000,0 45000.0 45O0000xli 008000 0,1000 00.8000 018000 0.8000ERAMI 190000 160000 1.0000 1,0000 110000

- ~ W839 0. 0. 0. 0w 0,PAMB 20139 2.139 21139 2.139 2,139TAMS 389.97 389.97 389097 389.97 389.97pa 3.0261 3.261 3.,261 39261 3,261T2 440.06 440.08 440.08 440r06 440.06PWSO 26997 2541.2 2124.6 1556.1 1107.3FPWSDI 3083.0 2885.2 23o6.b 1608.12 1062.2S'7C 0,3723 0.3719 0.3725 0.3827 0,4039ESFC 0.3248 0.3276 0.3431 0,3703 0,4133W7T 1001.4 945,1j 791'3 595,6 447.2FN 223.37 19S,42 103015 29.58 w14.24

12.la'ebo 126302 10.80 9.169 7,630XNL 11827, 11827. 10989. 9464e Was2P83 79.69 76.56 64.91 52.58 42086T93 1277.3 1259.5s 1187,4 1111s1 1042.?Pe 3.16b3 30.080 2.812 as565 2.442T61 1383.0 1359.3 1267.6 1192.4 1120.5

Page 82: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

aa TF34/T7 STUIDY Al **ESTIMATE PERFORMANCE LYNN MASS. APRIL 26, 1979

CASE 345.0000

ALT O.XM 0.ERAH4 1.0000W83g O.PAmB 14,696TAmB 549,47P2 14,696T2 549.47PwsD 7596.4EPWSO 8037.3SFC 094450

ESFC 0,4206WFT 3380.3FN 1102.20wI o3,997XNL 12173,PB$ 278,28TB3 1407.9P8 16.639

T6 1557o

IIII

I

I

Page 83: UNLASFIE UmhEEAhhhED ENGINE STUDY. GENERALDH47R LP turbine referred energy function Btu/lbm/°R I P47Q5 LP turbine pressure ratio ETL LP turbine adiabatic efficiency XNL LP turbine

U NCLASS IFET F1)

I) DST\I BUI1I ON L IST

REPORT NO. NAI)C-79133-60AIRTASK NO. A03P-03PA/O0i E/70880-001I WORK UNIT NO. )CM2O1

N N o._-of _!opies

-AVA IR..................................2(I for R. Brcvwn, AIR-330)j (I for J. Byers, ATR-53602)

DTC ................................... 12

NAVAIRPROPCEN. .. ..................................................

(I for R. Lazarick, PE-42)

NASA, Langley Research Center .. ................(1 for A. Reath, M/S 249A)

NASA, Lewis Research Center. ...................(I for B. Miller, M/S 301-2)

NASA, Headquarters .......................

(I for J. Madison, RJP-2)

INLSII