Wind Tunnel Test Results for Gas Flows Inside Axisymmetric Cavities on Cylindric Bodies with Nose Cones
Wind Tunnel Test Results for Gas Flows Inside Axisymmetric Cavities on Cylindric Bodies with Nose Cones
- New search for: Shvets, A. L.
- New search for: Gilinsky, M.
- New search for: Blankson, I. M.
- New search for: Shvets, A. L.
- New search for: Gilinsky, M.
- New search for: Blankson, I. M.
Experimental test results of air flow inside and at the cylindrical cavity located on axisymmetric body are presented. These tests were conducted in the wind tunnel A-7 of Institute of Mechanics at Moscow State University. Pressure distribution along the cavities and optical measurements were obtained. Dependence of these characteristics of length of a cavity in the range: L/D = 0.5 - 14 and free stream Mach in the range: M(sub infinity) = 0.6 - 3.0 was determined. Flow structure inside the cavity, cause of flow regime change, separation zones geometry and others were studied. In particular, the flow modes of with open and closed separation zones are determined.
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Wind Tunnel Test Results for Gas Flows Inside Axisymmetric Cavities on Cylindric Bodies with Nose Cones
AIAA 12th International Space Planes and Hypersonic Systems and Technologies Conference ; 2003 ; Norfolk, VA, United States
2004-01-01
Conference paper
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English