RamjetKerrebrock:

Path: ACPro/Airbreathing

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   Ramjet jet engine model producing thrust and specific fuel consumption. 
   Type RamjetKerrebrock for a demo.

   Since version 2014.1
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   Form:
 	[t, iSp, tS] =  RamjetKerrebrock( m, d, p )
   d =  RamjetKerrebrock;
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   ------
   Inputs
   ------
   m	(1,:)	Mach number
   d	(1,1)	Data structure for engine
           .gamma     (1,1) Specific heat ratio of air
           .cP        (1,1) Specific heat of air 
           .qR        (1,1) Heating value of fuel
           .tT4       (1,1) Temperature at station 4
           .aInlet    (1,1) Inlet area
   p   (1,1)	Standard atmosphere
            

   -------
   Outputs
   -------
   t 	 (1,:)	Thrust (N)
   iSp  (1,:)	Specific impulse (s)
   tS	 (1,:)	Specific thrust

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   Reference: Kerrebrock, J. 
   http://web.mit.edu/16.unified/www/FALL/thermodynamics/notes/node85.html
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Children:

Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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