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pro vyhledávání: '"W. J. Banning"'
Publikováno v:
8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Afterbody and base pressure measurements and flow visualization results are presented for a blunted conecylinder model rocket which had a centrally protruding nozzle. The model was mounted in supersonic free streams of Mach 2 and 3 produced by the De
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3b80661953706c824f6261fcec96200
https://doi.org/10.2514/6.1998-1598
https://doi.org/10.2514/6.1998-1598
