An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate into a Subsonic Free Stream.
ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE
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An experimental investigation of the surface static pressures on a flat plate due to a jet injecting transversely into a subsonic free stream was conducted. The free stream Mach numbers were 0.1, 0.2, 0.4, and 0.6 and the jet total pressure ranged from 0 to 1200 psig. The results are presented in tabular form with representative examples of the data shown graphically. Author
- Fluid Mechanics