Role of hydrogen/air chemistry in nozzle performance for a hypersonic propulsion system
Author:
Affiliation:
1. United Technologies Research Center, East Hartford, Connecticut 06108
2. Pratt and Whitney Aircraft, West Palm Beach, Florida 33410
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11495
Reference11 articles.
1. Estimates of oxides of nitrogen formed in a scramjet inlet
2. 2Vincenti, W. G., and Kruger, Jr., C. H. "Introduction to Physical Gas Dynamics," R. E. Krieger Publishing, Malabar, FL, 1965, pp.293-300.
3. Calculated chemical and vibrational nonequilibrium effects in hypersonic nozzles
4. LSODE and LSODI, two new initial value ordinary differential equation solvers
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