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1 School of Aerospace Engineering, Universiti Sains Malaysia, Engineering Campus, 14300 Nibong Tebal, Pulau Pinang, Malaysia 2 Institute No. 2 “Aviation, Rocket Engines and Powerplants”, Moscow Aviation Institute (National Research University), Volokolamskoe Shosse 4, 125993, Moscow, Russia 3 School of Mechanical Engineering, Universiti Sains Malaysia, Engineering Campus, 14300 Nibong Tebal, Pulau Pinang, Malaysia

The Impact of Streamwise Steps and Cavities Geometry on Supersonic Turbulent Boundary Layer