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NASA NTRS · 19660016279

Blunt slipstream calculation using the method of integral relations

Abstract

Compressible, inviscid secondary injection and primary flows calculated using integral relation method for blunt bodies - application to thrust vector control

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BibTeXRIS

Chenoweth, D. R.. 1965-04-01. Blunt slipstream calculation using the method of integral relations. https://ntrs.nasa.gov/citations/19660016279

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