Supersonic Flow of Chemically Reacting Gas-Particle Mixtures. Volume II. RAMP - A Computer Code for Analysis of Chemically Reacting Gas-Particle Flows

Most solid rocket motor propellants contain metal additives which increase the energy content of the system and also suppress combustion pressure instabilities. The presence of these metal additives, however, results in condensed products in the exhaust which can do no expansion work and thereby red...

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Bibliographische Detailangaben
Hauptverfasser:	Penny,Morris M, Smith,Sheldon D, Anderson,Peter G, Sulyma,Peter R, Pearson,Marcus L
Format:	Report
Sprache:	eng
Schlagworte:	Combustion and Ignition COMBUSTION PRODUCTS Computer Programming and Software COMPUTER PROGRAMS COMPUTERIZED SIMULATION EXHAUST GASES EXHAUST PLUMES FLOW FIELDS Fluid Mechanics PARTICLES RAMP computer program REACTION KINETICS ROCKET NOZZLES Solid Propellant Rocket Engines SUPERSONIC FLOW TRAN-72 computer program
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