NASA NTRS · 19990106575
Optimization of a GO2/GH2 Impinging Injector Element
Abstract
An 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.
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Tucker, P. Kevin, Shyy, Wei, Vaidyanathan, Rajkumar. 1999-01-01. Optimization of a GO2/GH2 Impinging Injector Element. https://ntrs.nasa.gov/citations/19990106575
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