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Unstructured Large Eddy Simulation of the passive control of the flow in a weapon bay
Authors:V Levasseur  P Sagaut  M Mallet  F Chalot
Institution:aInstitut Jean le Rond d’Alembert, Université Pierre et Marie Curie - Paris 6, 4 place Jussieu - case 162, 75252 Paris Cedex 05, France;bAircraft Technical Engineering and Loads Division, Dassault-Aviation, 78, quai Marcel Dassault, 92552 Saint-Cloud, France
Abstract:The control of cavity flows has been investigated by the means of Large Eddy Simulations. The computations have been carried out on unstructured meshes to assess the efficiency of two passive acoustic oscillation suppression devices: the rod-in-crossflow and the flat-top spoiler. Despite a sustained interest and many experiments, a clear explanation for observed reduction in the flow-induced structure load is still missing. This work explores different hypotheses: the modification of the mean field and its linear stability properties, a pure deflection effect of the separated shear layer, or scale coupling between the rod wake and the turbulent mixing layer over the cavity. The aim here is to enhance the experimental database and provide leads towards a better understanding of the phenomena. The selected test-case is a cavity of length/depth ratio equal to 5, at Mach and Reynolds number of M=0.85 and ReL=7.106, respectively.
Keywords:Large Eddy simulation  Rossiter aero–  acoustic mode  Flow control  Cavity flow  Turbulence
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