Hypersonic Transitional Shock-Wave–Boundary-Layer Interaction on a Flat Plate-Reference-Cited by-同舟云学术

Hypersonic Transitional Shock-Wave–Boundary-Layer Interaction on a Flat Plate

Published:2020-02 Issue:2 Volume:58 Page:814-829
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Currao Gaetano M. D.¹,Choudhury Rishabh²,Gai Sudhir L.¹,Neely Andrew J.¹,Buttsworth David R.²

Affiliation:

1. UNSW Canberra, Canberra, Australian Capital Territory 2612, Australia

2. University of Queensland, Brisbane, Queensland 4072, Australia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference39 articles.

1. Shock waves/turbulent boundary-layer interactions - Fundamental studies and applications

2. CurraoG. M. D. “Experimental Study of Hypersonic Fluid Structure Interaction with Shock Impingement on a Cantilevered Plate,” Ph.D. Thesis, Univ. of New South Wales–Canberra, Canberra, Australia, 2018.

3. Aerothermodynamics – A critical review at DLR

4. HirschelE.ClausW., Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, Vol. 229, Springer Science & Business Media, Berlin, 2009, pp. 13–37, Chap. 2.1.

5. On the görtler instability of boundary layers

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