High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets
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 ; 1501-1513
01.01.2009
13 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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Three-Dimensional Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets
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