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   <subfield code="a">Large-scale unsteadiness in a compressible, turbulent reattaching shear layer</subfield>
   <subfield code="h">[Elektronische Daten]</subfield>
   <subfield code="c">[J. Poggie, T. Leger]</subfield>
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   <subfield code="a">The large-scale unsteadiness that occurs in shock-wave/boundary layer interactions imposes severe aero-thermo-acoustic loads on high-speed aircraft. Much progress has been made on this problem in the last two decades: these interactions can now be tackled with large eddy simulation, at least for relatively low Reynolds numbers. Further, a large body of evidence now suggests that the physical mechanism for the unsteadiness lies in the selective amplification, within the separated flow, of large-scale disturbances originating in the incoming turbulent flow. The present paper examines the kinematics of these incoming structures in a turbulent boundary layer, and the scaling of the corresponding response of a reattaching shear layer flow. In particular, it presents an overview of the influence on recent research of experimental work carried out by Smits' group at Princeton University in the 1990s.</subfield>
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   <subfield code="a">• Springer-Verlag Berlin Heidelberg (outside the USA), 2015</subfield>
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