AirshipDrag:

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   Compute the approximate drag on an airship.
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   Form:
   D = AirshipDrag( h, u, A, Cd );
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   ------
   Inputs
   ------
   h           (1)       Altitude           [m]
   u           (1)       Velocity           [m/s]
   A           (1)       Reference Aera     [m^2]
   Cd          (1)       Zero-incidence drag coeffcient

   -------
   Outputs
   -------
   D           (1)       Total drag force   [N]

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Children:

Common: Atmosphere/StdAtm