A Unified Approach on Combustion Instability in Cryogenic Liquid Rocket Engines
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2009 ; Orlando, FL
47th AIAA Aerospace Sciences Meeting and the New Horizons Forum and Aerospace Exhibit 2009 ; 2483-2494
01.01.2009
12 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Aufsatz (Konferenz)
Englisch
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Physical Hypothesis for the Combustion Instability in Cryogenic Liquid Rocket Engines
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