35th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion and Energy

SPILLAGE DRAG REDUCTION IN DIVERTERLESS SUPERSONIC INLET

H. Miki¹, J. Akatsuka¹, R. Nimura, Tokyo University of Agriculture and Technology, Japan; ¹JAXA, Japan

This study investigates spillage drag reduction in diverterless supersonic inlets through CFD-based parametric analysis of bump and cowl shape. It also examines vortex generators installed upstream of the inlet as a complementary method to enhance drag reduction and mitigate boundary layer ingestion.


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DOI: 10.71945/icas2026_0418