Multiple-orifice liquid injection into hypersonic air streams.
- 1 December 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (12) , 1705-1707
- https://doi.org/10.2514/3.6714
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Flight Test Base Pressure Results at Hypersonic Mach Numbers in Turbulent FlowAIAA Journal, 1972
- Heat-transfer and ablation-rate correlations for reentry heatshield and nosetip applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Flight results showing the effect of mass addition on base pressureAIAA Journal, 1970
- Base pressure results at M equals 4 using free-flight and sting-supported models.AIAA Journal, 1968
- Study of penetration of a liquid injectant into a supersonic flow.AIAA Journal, 1968