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Optimization of a GO2/GH2 Impinging Injector ElementAn existing injector optimization methodology, method i, is used to investigate optimal design points for a GO2/GH2 impinging injector element. The impinging element, an F-O-F triplet, is optimized in terms of such relevant design variables as fuel pressure drop, DELTA-P(sub f), oxidizer pressure drop, DELTA-P(sub o), combustor length, L(sub comb), and impingement angle, alpha, for a given mixture ratio and chamber pressure.
Document ID
19990106575
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Tucker, P. Kevin
(NASA Marshall Space Flight Center Huntsville, AL United States)
Shyy, Wei
(Florida Univ. Gainesville, FL United States)
Vaidyanathan, Rajkumar
(Florida Univ. Gainesville, FL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop
Location: Huntsville, AL
Country: United States
Start Date: September 13, 1999
End Date: September 17, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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