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Path: ACPro/ACProAerodynamics
% Drag coefficient for subsonic, supersonic and hypersonic flight.
This combines subsonic, supersonic and hypersonic. All regimes
have a Mach number correction. The skin friction model is selectable.
If gamma is not entered it will be computed from p.
Type CD0Composite for a demo at an altitude of 1 km.
Since version 2014.1
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Form:
[cD0, cDW, cDF, cDP] = CD0Composite( m, d, alpha, p, gamma )
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Inputs
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m (1,:) Free stream Mach number
d (.) Data structure
.length (1,1) Characteristic length (m)
.oswaldEff (1,1) Oswald efficiency factor
.aspectRatio (1,1) Aspect ratio
.cDM1 (1,1) Drag coefficient at Mach 1
.mDD (1,1) Drag divergence Mach number
.thicknessRatio (1,1) Thickness to chord ratio
.model (1,:) Skin friction model
alpha (1,:) Angle of attack (rad)
p (.) Standard atmosphere data structure
gamma (1,1) Ratio of specific heats, optional
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Outputs
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cD0 (1,:) Drag coefficient
cDW (1,:) Wave drag
cDF (1,:) Skin friction drag
cDP (1,:) Pressure drag
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See also CDWave, CPHypersonic, CDSkinFriction
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ACPro: ACProAerodynamics/CDSkinFriction ACPro: ACProAerodynamics/CDWave ACPro: ACProAerodynamics/CPHypersonic AerospaceUtils: AtmosphericCalculations/AtmGamma Common: Atmosphere/StdAtm Common: Graphics/Plot2D
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