33th Congress of the International Council of the Aeronautical Sciences

03.1 - Aerodynamics – CFD Methods and Validation

NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS

D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy

In this work, we investigate the influence of high-temperature effects on compressible wall-bounded turbulence, by carrying out a DNS and LESs of a hypersonic turbulent flat-plate boundary layer, thermally and chemically out-of-equilibrium. The analysis aims at assessing the effects of thermochemical activity on turbulence, by means of a detailed investigation of turbulent statistics.


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