Path: ACPro/ACPerformance
% Computes the stall velocity.
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Form:
vStall = VStall( d, altitude )
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Inputs
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d (1,1) Data structure
.cLMax (1,1) Max lift coefficient
.wingArea (1,1) Wing area
.massDesign (1,1) mass
altitude (1,1) Altitude (m)
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Outputs
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vStall (1,1) Stall velocity
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Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance,"
Cambridge, p. 139.
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AerospaceUtils: AeroData/AtmData Common: Atmosphere/StdAtm Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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