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Publikováno v:
H. Lui, T. R. Ricciardi and W. R. Wolf and Carlos Junqueira-Junior. "Comparison of Shock-Boundary Layer Interactions in Adiabatic and Isothermal Supersonic Turbine Cascades," AIAA 2022-4133. AIAA AVIATION 2022 Forum. June 2022
Wall-resolved large eddy simulations are employed to investigate the shock-boundary layer interactions (SBLIs) in a supersonic turbine cascade. An analysis of the suction side separation bubbles forming due to the SBLIs is presented for adiabatic and
Externí odkaz:
http://arxiv.org/abs/2301.01577