NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Transverse injection of a particle-laden liquid jet in supersonic flow: A three-phase flowThe results of a two part study of the behavior of particle laden liquid jets injected into air are presented. Water was used as the liquid carrier and either 1-37 or 13-44 microns diam. spherical glass beads with a specific gravity of 2.8-3.0 as the particles. The observations were mainly photographic. The breakup of jets injected into still air was investigated as a function of particle loading, and the results were compared to the pure liquid jet case. The jets were found to be more stable with particles present. The length to breakup was increased, and the formation of satellite droplets was suppressed. The penetration and breakup of transverse jets in a Mach 3.0 air stream was studied. The general breakup mechanism of wave formation was found to be the same as for the all liquid case. Significant separation of the phases was observed, and the penetration of the liquid phase was reduced compared to all liquid cases at the same value of the jet to free stream momentum flux ratio.
Document ID
19810007769
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schetz, J. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Ogg, J. C.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
August 11, 2013
Publication Date
November 1, 1980
Publication Information
Publication: NASA. Langley Research Center The 17th JANNAF Combust. Meeting, Vol. 1
Subject Category
Propellants And Fuels
Accession Number
81N16285
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available