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What is Compressibility in Supersonic Turbulent Layers about?

This study examines compressibility effects in supersonic and hypersonic turbulent boundary layers influenced by wall disturbances, utilizing direct numerical simulation at Mach numbers up to 6. The findings indicate that wall disturbances intensify turbulent motions and significantly affect Reynolds stresses and mean velocity, with notable contributions from density fluctuations. The research also explores the organization of dilatational motions and their limited impact on skin friction and turbulent kine

Author

hdhcbchkahh

Language

EN