Numerical Modelling of Ramjet Combustors.
Final rept. Oct 81-Aug 82,
AIR FORCE WRIGHT AERONAUTICAL LABS WRIGHT-PATTERSON AFB OH
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The present work deals with development of computer codes for modelling of gas turbine combustors to ramjet combustor configurations. In particular, the STARPIC code of Lilley and Rhode has been expanded to include reacting compressible flows. Author
- Jet and Gas Turbine Engines