Problem of diffusion from hypersonic velocities is of importance in design of hypersonic air-breathing propulsion systems, since way in which diffusion is accomplished has important effect in determining overall performance of system; criteria of performance of hypersonic air intakes are defined as consisting of efficiency and capability; required geometry variation to maintain shock on lip condition for 2 intakes is shown.
Intakes for hypersonic ramjets
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 9 , n 7
1963
2 pages
Aufsatz (Zeitschrift)
Englisch
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