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Dominique Bauer Department of Construction Engineering July 15, 2004 Using the TI voyage 200 In Structural Analysis
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Using the TI voyage 200 In Structural Analysis - RFDZrfdz.ph-noe.ac.at/fileadmin/Mathematik_Uploads/ACDCA/TIME2004/tim… · Using the TI voyage 200 In Structural Analysis. ... SFD

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Page 1: Using the TI voyage 200 In Structural Analysis - RFDZrfdz.ph-noe.ac.at/fileadmin/Mathematik_Uploads/ACDCA/TIME2004/tim… · Using the TI voyage 200 In Structural Analysis. ... SFD

Dominique BauerDepartment of Construction Engineering

July 15, 2004

Using the TI voyage 200In Structural Analysis

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Structural AnalysisTI voyage 200

• Examples in Structural Analysis will be presented that illustrate the use of the TI voyage 200, a symbolic and graphic calculator.

• The examples are taken from a first course in Structural Analysis at the undergraduate level. They deal with classical methods of analysis for both statically determinate and statically indeterminate structures.

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Structural AnalysisTI voyage 200

• The use of the TI voyage 200 greatly reduces the mathematical difficulties in problem solving, and thus allows the students to spend more time in developing a good understanding of the behaviour of structures.

• The TI voyage 200 is a complex tool and the examples illustrate how to use the calculator in such a way that the students will want to take advantage of its computational power throughout their careers in structural engineering.

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Structural AnalysisTI voyage 200

• The examples are taken from a textbook used in Structural Analysis at the École de technologie supérieure (Samikian,1994).

• The examples are an attempt to update the contents of the textbook by including the use of a symbolic calculator. The have been developed over the last four years by the speaker. Presently, they are part of the class notes and eventually will be included in a new edition of the textbook.

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Structural AnalysisTI voyage 200

• Three-Hinged Arch (Samikian, example 2.4)

– System of linear simultaneous equations

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Example 2.4

Determine the support reactions for the three-hinged arch shown in the Figure below.

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20 20 (80 10) 0C y xM A A= − − × =∑

40 (80 30) 0B yM A= − × =∑

0x x xF A B= − =∑

80 0y y yF A B= + − =∑

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solve(20ay-20ax-800=0 and 40ay-2400=0 and ax-bx=0 and ay+by-80=0,{ax,ay,bx,by})

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ax = 20.0 and ay = 60.0 and bx = 20.0 and by = 20.0

20 kN60 kN

20 kN20 kN

x

y

x

y

AA

BB

==

==

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20 20 80040 2400

080

x y

y

x x

y y

A AA

A BA B

− + =+ =

− =+ =

[ ]{ } { }A x B=

simult(a,b)

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[ ]

20 20 0 00 40 0 01 0 1 00 1 0 1

A

− = −

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{ }

8002400

080

B

=

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Structural AnalysisTI voyage 200

Parabolic Cables (Samikian, example 4.4)

– System of non linear simultaneous equations

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Example 4.4

Determine the maximum tension in a cable under a uniform load of 12 kN/m, for the geometry shown in Figure 4.12.

Figure 4.12

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Figure 4.13

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From Equation 2.8, we have for the left-hand part

2

10 02A

wxM H= − + =∑For the right-hand part, we have

2( )30 02B

w L xM H −= − =∑

From Equation 2.7, we have for the left-hand part

0y AF V wx= − =∑For the right-hand part, we have

( ) 0y BF V w L x= − − =∑

(1)

(2)

(3)

(4)

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solve(-10h+w*x^2/2=0 and30h-w*(1-x)^2/2=0 and va-w*x=0 andvb-w*(l-x)=0,{x,h,va,vb})|w=12 and l=80

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x = 29.3 and h = 514.5 and va = 351.4 and vb = 608.6orx = -109.3 and h = 7165.5 and va = -1311.4 and vb = 2271.4

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Therefore, we find

29.3, 514.5, 351.4, 608.6or

109.3, 7165.5, 1311.4, 2271.4

A B

A B

x H V V

x H V V

= = = =

= − = = =

where only the first solution has physical meaning.

Finally,

( ) ( ) ( ) ( )2 2 2 2351,4 514,4 623 kNA AT V H= + = + =

et

( ) ( ) ( ) ( )2 2 2 2608.6 514.4 796.9 kNB BT V H= + = + =

The maximum tension in the cable is at support B, with the highest elevation.

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Structural AnalysisTI voyage 200

• Method of Virtual Work (Samikian, chapter 9)

– Symbolic calculations, Mohr’s integrals

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The work done by the virtual load undergoing the real displacement

is equal to

the work done by the virtual internal forces undergoing the real internal deformations

01

L Mm dxEI

⋅∆ = ∫

Real Displacement Real Internal Deformation

Unit Virtual Load Virtual Internal Moment

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Example

Find the deflection at point C

La b

A C B

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L

A B

w : real load

2AwLR =

2BwLR =

V

2wL

M2

max 8wLM =

2

2 2wLx wxM = −

2wL

SFD

BMD

FBD x

x

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A B

1 : unit virtual load

AbRL

= BaRL

=

m

maxabmL

=

( )am L xL

= −

La b

bxmL

=

BMD

FBD x

x

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( )

2

2 2

, 0

,

wLx wxM

bxm x aLam L x a x LL

= −

= ≤ ≤

= − ≤ ≤

01

L

CMm dxEI

⋅∆ = ∫

( )

2

0

2

( )2 2

2 2

a

C

L

a

L a x wLx wx dxL

a wLx wxL x dxL

−∆ = − +

− −

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( )

2

0

2

( )2 2

2 2

a

L

a

L a x wLx wx dxL

a wLx wxL x dxL

−− +

− −

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2La =When

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Mohr’s Integrals

Reference : « Techniques de l’ingénieur », Construction Series, Volume C5, Chapter C2555

0

1 Mmdx∫

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Structural AnalysisTI voyage 200

• Coordinate Transformations

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x2

y2

θ

x1

y1

F

P1

V1

– P1 sin θ

P1 cos θ

V1 cos θ

V1 sin θ

P1 cos θ + V1 sin θ

– P1 sin θ + V1 cos θ

Coordinate Transformations

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The transf(p1,v1,θ) program transforms the components (p1,v1) of a vector defined in the x1y1 Cartesian coordinate system into components (p2,v2) in the x2y2 Cartesian coordinate system.

The x2y2 coordinate system makes an angle θwith the x1y1 system, where θ is positive when measured anticlockwise.

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1.Download the transf program(file : transf.9xp) from the Web site onto your computer

2.Transfer the transf program from your computer to the calculator usingTI Connect (USB cable) or TI-Graph Link (serial cable)

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3.Once the program is loaded in the calculator, give the command transf(p1,v1,θ). In the following example, p1=10, v1=10*2=20 and θ = 30°.

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The program displays the values of p1, v1, θ and p2, v2. Also, a drawing is shown for checking purposes.

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(p1,v1,θ)Prgm

√(p1^2+v1^2)→f

tan(v1/p1)→α

p1*cos(θ)+v1*sin(θ)→p2

⁻p1*sin(θ)+v1*cos(θ)→v2

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ClrDrawsetGraph("axes","off")

max({p1,v1,p2*cos(θ),p2*sin(θ),⁻v2*sin(θ),v2*cos(θ)})→gmax

min({p1,v1,p2*cos(θ),p2*sin(θ),⁻v2*sin(θ),v2*cos(θ)})→gmin

max(abs(gmax),abs(gmin))→gmax

⁻1.2*gmax→xmin

⁻1.2*gmax→ymin

1.2*gmax→xmax

1.2*gmax→ymax

ZoomSqr

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PxlText "p1="&string(p1),5,0PxlText "v1="&string(v1),15,0PxlText " f="&string(f),25,0PxlText " α="&string(α),35,0

PxlText "θ="&string(θ),50,0PxlText "p2="&string(p2),60,0PxlText "v2="&string(v2),70,0

PxlText "(c)2003",83,0PxlText "D.Bauer",93,0

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Line 0,0,p1,v1Line 0,0,p1,0Line 0,0,0,v1

PtText string(p1),p1,0PtText string(v1),0,v1

Pause

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Line 0,0,p2*cos(θ),p2*sin(θ)Line 0,0,⁻v2*sin(θ),v2*cos(θ)

PtText string(p2),p2*cos(θ),p2*sin(θ)PtText string(v2),⁻v2*sin(θ),v2*cos(θ)

Pause

setGraph("axes","on")DispHomeEndPrgm

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Structural AnalysisTI voyage 200

• Acknowledgments– The present research was made possible by

grants from the École de technologie supérieure (PSIRE-ENS 2001,2003).