Measurements of OH and H2O for reacting flow in a supersonic combusting ramjet combustor
- 1 November 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 11 (6) , 1154-1161
- https://doi.org/10.2514/3.23954
Abstract
No abstract availableKeywords
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