Tests were conducted in University of Michigan 8 × 13-in. supersonic tunnel at 3.97 Mach and 0.12 × 106/in. Re; test model consisted of wedge of rectangular planform equipped with side plates and fullspan jet slot near base; primary data taken were jet mass flow, normal force increment due to jet, and schlieren photographs; for range of variables covered, momentum flux ratio was found to govern flow geometry, including location of transition in separated shear layer; data on aerodynamic interaction in case of approximately 2-dimensional slot-jet configurations were collected from four sources.
Two-dimensional secondary jet interaction with supersonic stream
AIAA J
AIAA Journal ; 5 , n 4 ; p 655-670
1967
16 pages
Aufsatz (Zeitschrift)
Englisch
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