Path: ACPro/ACPerformance
% Returns Concorde properties.
The SFC and F/delta are only valid between M = 1 and M = 2.
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Form:
d = ConcordeProperties( machNo )
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Inputs
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machNo (1,1) Mach number
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Outputs
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d (1,1) Aircraft parameters
.massDry (1,1)
.massFuel (1,1)
.massDesign (1,1) Design point for calculations
.sFC (1,:) Specific fuel consumption
.cL (1,:) Lift coefficient
.cD (1,:) Drag coefficient
.k1 (1,:) Drag polar coefficient 1
.k2 (1,:) Drag polar coefficient 2
.wingArea (1,1) Wing area (m^2)
.wingLoading (1,1) Wing loading
.name (1,:) Name
.cLCoeff (1,1) Lift coefficient
.cLMax (1,1) Maximum lift coefficient
.fOverDelta (1,:) Force over P/P0
def {:,3} Property definitions
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Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance,"
Cambridge, pp. 167-168.
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ACPro: ACProAerodynamics/ConcordeLD 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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