Supersonic combustion of hydrogen in a vitiated air stream using stepped-wall injection
Author:
Affiliation:
1. NASA, LEWIS RESEARCH CENTER, CLEVELAND,OHIO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1971-721
Reference18 articles.
1. Fuel injection and mixing in a supersonic stream
2. Schlichting, H., Boundary Layer Theory, HcGraw-Hill, New York. 1955, pp.502-508.
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