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The Effect of Diamond Injector Geometry on Supersonic Jet Interaction Secondary Flow

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Pubblicato in:44th AIAA Aerospace Sciences Meeting and Exhibit; Reno, NV; USA; 9-12 Jan. 2006 (Jan 9, 2006), p. 1-17
Autore principale: McLellan, Justin
Altri autori: Srinivasan, Ravichandra, Bowersox, Rodney D W
Pubblicazione:
American Institute of Aeronautics and Astronautics, 1801 Alexander Bell Drive, Suite 500, Reston, VA, 20191-4344, USA, [URL:http://www.aiaa.org]
Soggetti:
Supersonic jet flow
Flow characteristics
Secondary flow
Gas injection
High Mach number
Shock wave profiles
Jet interaction
Supersonic aircraft
Reynolds averaged Navier-Stokes method
Injectors
Near fields
Flow turning
Accesso online:Citation/Abstract
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