EngineExample:

Path: ACPro/Airbreathing

% Example engine parameters. Returns a data structure.
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   Form:
   d = EngineExample( type )
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   ------
   Inputs
   ------
   type      (1,:) 'turbofan', 'ramjet'

   -------
   Outputs
   -------
   d         (1,1)  Data structure

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   Reference:	Mattingly, "Elements of Gas Turbine Propulsion," 
               McGraw-Hill, 1996.
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Children:

AerospaceUtils: AeroData/AtmData

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