AbstractThe following paper reports on experimental investigations on high-speed missile control. The paper looks especially at the interference effects of side jets with supersonic cross flow. Detailed wall pressure measurements are presented for three different jet configurations. The shock structure is shown with Schlieren images and the wall streamlines are visualised with oil flow technique.
Experimental investigation of side jet interaction with a supersonic cross flow
Aerospace Science and Technology ; 12 , 4 ; 269-275
2007-01-24
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Experimental investigation of side jet interaction with a supersonic cross flow
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