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Computer Modeling Of AtomizationImproved mathematical models based on fundamental principles of conservation of mass, energy, and momentum developed for use in computer simulation of atomization of jets of liquid fuel in rocket engines. Models also used to study atomization in terrestrial applications; prove especially useful in designing improved industrial sprays - humidifier water sprays, chemical process sprays, and sprays of molten metal. Because present improved mathematical models based on first principles, they are minimally dependent on empirical correlations and better able to represent hot-flow conditions that prevail in rocket engines and are too severe to be accessible for detailed experimentation.
Document ID
19940000358
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Giridharan, M.
(CFD Research Corp.)
Ibrahim, E.
(CFD Research Corp.)
Przekwas, A.
(CFD Research Corp.)
Cheuch, S.
(CFD Research Corp.)
Krishnan, A.
(CFD Research Corp.)
Yang, H.
(CFD Research Corp.)
Lee, J.
(CFD Research Corp.)
Date Acquired
August 16, 2013
Publication Date
July 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-28721
Accession Number
94B10358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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