Discussion on Supersonic Combustion

  • A. Kumar
  • M. Y. Hussaini
Part of the ICASE/NASA LaRC Series book series (ICASE/NASA)


I work at the University of California. Lore of the sixties was that these engines could not afford normal shocks and yet in very much of your presentation you emphasized perpendicular injection. Is that lore correct?


Mach Number Hydrocarbon Fuel Normal Shock Supersonic Combustion Flight Mach Number 
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Copyright information

© Springer-Verlag, New York, Inc. 1992

Authors and Affiliations

  • A. Kumar
  • M. Y. Hussaini

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