Leading-edge bluntness effects on hypersonic three-dimensional flows over a compression ramp

Journal of Fluid Mechanics, vol. 923

Abstract

Abstract

Authors 6

1. Shibin Cao corresponding Aachen Shock Wave Laboratory

   Hong Kong Polytechnic University · RWTH Aachen University

   Affiliation as printed

   Department of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic University, Kowloon, Hong Kong

   Shock Wave Laboratory, RWTH Aachen University, 52056 Aachen, Germany

2. Jiaao Hao

   Hong Kong Polytechnic University

   Affiliation as printed

   Department of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic University, Kowloon, Hong Kong

3. Igor Klioutchnikov Aachen Shock Wave Laboratory

   RWTH Aachen University

   Affiliation as printed

   Shock Wave Laboratory, RWTH Aachen University, 52056 Aachen, Germany

4. Herbert Olivier Aachen Shock Wave Laboratory

   RWTH Aachen University

   Affiliation as printed

   Shock Wave Laboratory, RWTH Aachen University, 52056 Aachen, Germany

5. Karl Alexander Heufer Aachen Shock Wave Laboratory

   RWTH Aachen University

   Affiliation as printed

   Shock Wave Laboratory, RWTH Aachen University, 52056 Aachen, Germany

6. Chih‐Yung Wen

   Hong Kong Polytechnic University

   Affiliation as printed

   Department of Aeronautical and Aviation Engineering, The Hong Kong Polytechnic University, Kowloon, Hong Kong