Flow Control Effectiveness at High Speed Flows

Details Flow Control Effectiveness at High Speed Flows Flow Control Effectiveness at High Speed Flows

Feb 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005esasp.563..609k&link_type=abstract

Proceedings of the Fifth European Symposium on Aerothermodynamics for Space Vehicles (ESA SP-563). 8-11 November 2004, Cologne,

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Scientific paper

The effects of two important flow control techniques, i.e. jet control and dimples, on the aerodynamic characteristics and performance of a number of body configurations have been studied experimentally. The dimple studies have been carried out in a transonic-supersonic wind tunnel and the jet studies in a hypersonic gun tunnel at a Mach number of 8.2. Air was used as the working gas. The tests employed schlieren photography and oil-flow to study the overall flow field. Quantitative studies have been made by pressure measurements.

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