NDLI: Shear coaxial injector atomization phenomena for combusting and non-combusting conditions

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Shear coaxial injector atomization phenomena for combusting and non-combusting conditions

Content Provider	NASA Technical Reports Server (NTRS)
Author	Foust, M. J. Santoro, R. J. Ryan, H. M. Pal, S. Moser, M. D.
Copyright Year	1992
Description	Measurements of LOX drop size and velocity in a uni-element liquid propellant rocket chamber are presented. The use of the Phase Doppler Particle Analyzer in obtaining temporally-averaged probability density functions of drop size in a harsh rocket environment has been demonstrated. Complementary measurements of drop size/velocity for simulants under cold flow conditions are also presented. The drop size/velocity measurements made for combusting and cold flow conditions are compared, and the results indicate that there are significant differences in the two flowfields.
File Size	1052928
Page Count	39
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19940007054
Archival Resource Key	ark:/13960/t3hx6837w
Language	English
Publisher Date	1992-01-01
Access Restriction	Open
Subject Keyword	Fluid Mechanics And Heat Transfer Mixing Injectors Hydrogen Liquid Rocket Propellants Combustible Flow Drop Size Probability Density Functions Particle Size Distribution Vaporizing Liquid Oxygen Flow Distribution Laser Interferometry Coaxial Flow Thrust Chambers Flow Velocity Cold Flow Tests Hydrogen Oxygen Engines Atomizing Gaseous Rocket Propellants Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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