Scramjet engine/airframe integration methodology currently in use at the NASA Langley Research Center for design/analysis of hypersonic airbreathing vehicles is presented with illustrative example applications. The matrix encompasses engineering and higher order numerical methods that cover the major disciplines as well as a multidiscipline design/optimization approach.
Scramjet Engine/Airframe Integration Methodology
01.12.1997
Aufsatz (Konferenz)
Keine Angabe
Englisch
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