Variable turbulent prandtl number model for shock/boundary-layer interaction

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[1] [1,Roy, Subhajit

[2] 1,Pathak, Utkarsh

[3] 1,Sinha, Krishnendu

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| 1600年 / AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States卷 / 56期

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[32] TURBULENT BOUNDARY-LAYER INTERACTION WITH A SHOCK WAVE AT A COMPRESSION CORNER.
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[33] THE TRANSONIC INTERACTION OF A NORMAL SHOCK WITH A MILDLY SEPARATED TURBULENT BOUNDARY-LAYER
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[34] ON UPSTREAM INFLUENCE IN SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION
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[35] Shock-wave/turbulent boundary-layer interaction with a flexible panel
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[37] OBLIQUE SHOCK-WAVE - TURBULENT BOUNDARY-LAYER INTERACTION WITH SUCTION
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[39] THE INTERACTION BETWEEN AN OBLIQUE SHOCK-WAVE AND A TURBULENT BOUNDARY-LAYER
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[40] CALCULATION OF TURBULENT BOUNDARY-LAYER SHOCK-WAVE INTERACTION - COMMENT
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