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NASA NTRS · 19650031862

Integral approach to the yawed blunt body problem.

Abstract

Inviscid gas flow over nose region of supersonic yawed axisymmetric blunt body treated by integral relations in body oriented coordinate system

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BibTeXRIS

Waldman, G. D.. 1965-01-01. Integral approach to the yawed blunt body problem.. https://ntrs.nasa.gov/citations/19650031862

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