AirshipMaxCruise:
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Evaluate the maximum velocity and thrust for the airship throughout its
altitude range. The maximum velocity and thrust are computed based upon
the assumption that thrust = drag at the maximum velocity, with a
constant power limit applied throughout.
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Form:
[llh,ra,rEF,t] = DASim( x0, d, hMin );
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Inputs
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Cd0 (1,1) Zero angle drag coefficient
Vol23 (1,1) Reference area, volume^(2/3) (m^2)
Pmax (1,1) Maximum available power (W)
h (1,N) Altitude vector (m)
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Outputs
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Vmax (1,N) Maximum velocity at each altitude
Tmax (1,N) Maximum required thrust at each altitude
q (1,N) Max dynamic pressure at each altitude
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Children:
Common: Graphics/NewFig
