AirshipCoefficients:

Path: Airships/Modeling

% Load the approximate aerodynamic coefficients for an airship.

   Includes drag coefficients for hull, fins and gondola, and lift
   coefficients for the fins.
--------------------------------------------------------------------------
   Form:
   d = AirshipCoefficients;
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   none

   -------
   Outputs
   -------
   d           (.)       Data structure containing aerodynamic coefficients

--------------------------------------------------------------------------

Back to the Airships Module page