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NASA NTRS ยท 19700047128

Interaction shock shape for transverse injection in supersonic flow

Abstract

Interaction shock shape prediction for gaseous and liquid injection in supersonic flow, using solid body and complementary models

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BibTeXRIS

Schetz, J. A.. 1970-02-01. Interaction shock shape for transverse injection in supersonic flow. https://ntrs.nasa.gov/citations/19700047128

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