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F4U Corsair Kevin Dean, Jon Ramba, Tyler McCall Configuration Aerodynamics March 30, 2005
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F4U Corsair - Virginia Techmason/Mason_f/F4US05.pdf · F4U Corsair Kevin Dean, Jon Ramba, Tyler McCall Configuration Aerodynamics March 30, 2005

Jan 29, 2021

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  • F4U Corsair

    Kevin Dean, Jon Ramba, Tyler McCallConfiguration Aerodynamics

    March 30, 2005

  • History

    Carrier-based fighter- February, 1938

    Designed by 6 men

    First Flight – May 1,1940

    Used the mostpowerful engine inthe world at that time,producing over 2000hp

    (nicosfly.free.fr)

  • History

    Over 12,500produced

    Less than 30 stillairworthy today

    Had a kill:death ratioof 11.3

    (www.aoqz76.dsl.pipex.com)

  • Performance (F4U-1)

    Max Speed: 417 mph

    Cruise Speed: 182 mph

    Ceiling: 36,900 ft

    Max Range: 1,560 mi

  • Basic Geometry

    Wing Span: 41 ft

    Length: 33 ft 4 in.

    Height: 16 ft 1 in.

    Wing area: 314 ft2

    Aspect Ratio: 5.5

  • Basic Geometry

    Taper Ratio: 0.68

    Tail Scrape Angle: 23.1°

    Wetted Area: 1045 ft2

    Tail Span: 16.6 ft

    St/Sref: 0.22

  • Weights

    Empty Weight: 8982 lbs

    TOGW: 14000 lbs

    Max Fuel: 537 gals (3222 lbs)

    Wpayload/TOGW: 0.1283

    WFuel/TOGW: 0.2301

    Wing Loading: 28.5 lb/ft2

  • Neutral Point

    CG approx. 10 ft from nose

    Neutral Point = 14 ft

    Cm/CL = -0.5272

    Load split for trimmed cruise: 67.7 % on wing

    32.3 % on tail

  • Propulsion System

    Pratt-Whitney R-2800-18W DoubleWasp 18 cylinderradial engine

    2000 hp @ 2700rpm

    (www.aviation-history.com)

  • Aerodynamic Data

    NACA 2415 Airfoil

    t/c = 15 %

    (otterpop.sbay.org)

  • Aerodynamic Data

    28.365L/Dmax

    0.2759CL at L/Dmax

    Weight = 9000 lbs

    22.212L/Dmax

    0.3523CL at L/Dmax

    Weight = 11491 lbs

    18.233L/Dmax

    0.4292CL at L/Dmax

    Weight = TOGW = 14000 lbs

    Using cruise speed 182 mph at sea level and assume straightand level flight (L=W)

    23.985L/Dmax

    0.326CL at L/Dmax

    Using the FRICTION (Very Rough Estimate) and Cruisespeed 182 mph at sea level

    CALCULATED PERFORMANCE

  • Control Surfaces

    0.354b/bREF

    0.2197S/SREF

    RUDDER

    0.365b/bREF

    0.062S/SREF

    AILERONS

    0.46b/bREF

    0.223S/SREF

    FLAPS

    0.941b/bREF

    0.6028S/SREF

    ELEVATORS

  • Armament

    Six .50 calibermachine guns

    2 1000 lb bombsOR 8 5 in. rockets

    (www.aviation-history.com)

  • References

    Swinhart, Earl (http://www.aviation-history.com/vought/f4u.html)

    Tillman, Barrett. Corsair, The F4U inWorld War II and Korea. NavalInstitute Press, (1979)

    Mason, William(http://www.aoe.vt.edu/~mason/Mason_f/MRsoft.html)