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NASA NTRS · 19650045502

Inviscid hypersonic flow around blunt bodies.

Abstract

Nonequilibrium flow, angles of attack and vapor injection effects on subsonic flow field of blunt body

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BibTeXRIS

Kaattari, G. E., Katzen, E. D.. 1965-07-01. Inviscid hypersonic flow around blunt bodies.. https://ntrs.nasa.gov/citations/19650045502

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