[E-5] Plasma Flows

[2022-e-21] Experimental and numerical study on plasma-assisted rapid control of flowfield around nose of hypersonic transport

*Yasumasa Watanabe¹, Kojiro Suzuki² (1. Department of Aeronautics and Astronautics, The University of Tokyo, 2. Department of Advanced Energy, The University of Tokyo)

キーワード：Plasma-assisted flow control, Hypersonic, Wind tunnel test