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

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Detaylı Bibliyografya
Yayımlandı:	44th AIAA Aerospace Sciences Meeting and Exhibit; Reno, NV; USA; 9-12 Jan. 2006 (Jan 9, 2006), p. 1-17
Yazar:	McLellan, Justin
Diğer Yazarlar:	Srinivasan, Ravichandra, Bowersox, Rodney D W
Baskı/Yayın Bilgisi:	American Institute of Aeronautics and Astronautics, 1801 Alexander Bell Drive, Suite 500, Reston, VA, 20191-4344, USA, [URL:http://www.aiaa.org]
Konular:	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
Online Erişim:	Citation/Abstract
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