30th Congress of the International Council of the Aeronautical Sciences

02.3 - Basic Fluid Dynamics and Flow Control

STUDY OF THE UNSTEADY STRUCTURES EVOLUTION IN SHOCK WAVE / BOUNDARY LAYER INTERACTION FOR VARIOUS UPSTREAM CONDITIONS

P.A. Polivanov¹, A.A. Sidorenko¹, A.A. Maslov¹; ¹ITAM SB RAS, Russia

The paper deals with an experimental and numerical study of the upstream boundary layer state on characteristics of the SWBLI and the wake. The experimental data provide the database for verification of turbulence models for transitional RANS computations. The flow control devices damping growth of the momentum thickness were studied.


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