NASA NTRS · 19710044823
Injector design criteria using noncircular orifice geometry
Abstract
Rocket engine propellant injectors with noncircular orifice geometry, presenting experimental spray patterns and predicted performance for noncircular and circular orifice configurations
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Clapp, S. D., Mchale, R. M., Nurick, W. H.. 1971-04-01. Injector design criteria using noncircular orifice geometry. https://ntrs.nasa.gov/citations/19710044823
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