Computer program for estimation of leading-edge suction distribution for plane thin wings at subsonic speeds.
Abstract:ESDU 94038 introduces a Fortran program, ESDUpac A9438, that calculates the total theoretical leading-edge suction and its normalised spanwise distribution for wings from the tabulated values for the distribution given in ESDU 94037, making any necessary interpolations. It applies to wings with unswept or swept back leading-edges. The input to and output from the program are explained and illustrated by a worked example.
|Data Item ESDU 94038|
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- Aircraft Noise
- Fatigue - Endurance Data
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- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
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- Stress and Strength
- Transonic Aerodynamics
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