Incompressible/compressible/hypersonic flow-II

[9-D-04] Influence of Ablation on Laminar-Turbulent Transition over Compression Ramp at Mach 8

*Ata Onur Baskaya¹, Stefan Hickel¹ (1. Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherlands)

キーワード：Hypersonic flow, Laminar-turbulent transition, Ablation