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Steady longitudinal vortices in supersonic turbulent separated flows

Published online by Cambridge University Press:  04 March 2011

ERICH SCHÜLEIN  and
VICTOR M. TROFIMOV
ERICH SCHÜLEIN*
Affiliation:
Department of High Speed Configurations, German Aerospace Center DLR, Institute of Aerodynamics and Flow Technology, Bunsenstr. 10, 37073 Göttingen, Germany
VICTOR M. TROFIMOV
Affiliation:
Department of Technology, Novosibirsk State Pedagogical University, ul. Viluyskay 28, 630126 Novosibirsk, Russia
*
†Email address for correspondence: erich.schuelein@dlr.de
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Abstract

Large-scale longitudinal vortices in high-speed turbulent separated flows caused by relatively small irregularities at the model leading edges or at the model surfaces are investigated in this paper. Oil-flow visualization and infrared thermography techniques were applied in the wind tunnel tests at Mach numbers 3 and 5 to investigate the nominally 2-D ramp flow at deflection angles of 20°, 25° and 30°. The surface contour anomalies have been artificially simulated by very thin strips (vortex generators) of different shapes and thicknesses attached to the model surface. It is shown that the introduced streamwise vortical disturbances survive over very large downstream distances of the order of 104 vortex-generator heights in turbulent supersonic flows without pressure gradients. It is demonstrated that each vortex pair induced in the reattachment region of the ramp is definitely a child of a vortex pair, which was generated originally, for instance, by the small roughness element near the leading edge. The dependence of the spacing and intensity of the observed longitudinal vortices on the introduced disturbances (thickness and spanwise size of vortex generators) and on the flow parameters (Reynolds numbers, boundary-layer thickness, compression corner angles, etc.) has been shown experimentally.

JFM classification

Boundary Layers: Free shear layers Aerodynamics: High-speed flow
Type
Papers
Information
Journal of Fluid Mechanics , Volume 672 , 10 April 2011 , pp. 451 - 476
Copyright
Copyright © Cambridge University Press 2011

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References

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