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Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
The aerodynamics and the stability and control characteristics of a hypersonic vehicle that is has an un-started inlet are addressed. The vehicle considered is a generic scramjetpowered ∞ight test vehicle with a 3D, inward-turning inlet and crucifo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ee4a4f7fec07273057b43c88308d755
https://doi.org/10.2514/6.2009-7292
https://doi.org/10.2514/6.2009-7292
