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NASA NTRS · 19700057449

Injector design criteria using noncircular orifice geometry

Abstract

Liquid rocket engine injector elements design criteria, using noncircular orifice geometry to predict efficiency

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BibTeXRIS

Clapp, S. D., Mchale, R. M., Nurick, W. H.. 1970-06-01. Injector design criteria using noncircular orifice geometry. https://ntrs.nasa.gov/citations/19700057449

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