EFFECTS OF EXHAUST NOZZLE RECOMBINATION ON HYPERSONIC RAMJET PERFORMANCE
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1995
Reference18 articles.
1. Nonequilibrium Expansions of Air with Coupled Chemical Reactions
2. COMPLEX CHEMICAL KINETICS IN SUPERSONIC NOZZLE FLOW
3. KINETICS OF HYDROGEN-AIR FLOW SYSTEMS. II. CALCULATIONS OF NOZZLE FLOWS FOR RAMJETS
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