Influence of Boundary-Layer State on Development Downstream of Normal Shock Interactions-Reference-Cited by-同舟云学术

Influence of Boundary-Layer State on Development Downstream of Normal Shock Interactions

Published:2018-06 Issue:6 Volume:56 Page:2298-2307
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Davidson Todd S. C.¹,Babinsky Holger¹

Affiliation:

1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom

Funder

FP7 Transport

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056567

Reference42 articles.

1. AckeretJ.FeldmanF.RottN. “Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed,” Technical Memorandum 1113, Das Institut für Aerodynamik an der Eidgenössischen Technischen Hochschule, Zurich, Switzerland, 1947.

2. Shock wave/turbulent boundary layer interaction and its control

3. Transonic Shock Wave???Boundary-Layer Interactions

4. GaddG. E. “Interactions Between Normal Shock Waves and Turbulent Boundary Layers,” Repts. & Memoranda 3262, National Physical Inst., Teddington, U.K. 1961.

5. SawyerW. G.LongC. J. “A Study of Normal Shock-Wave Turbulent Boundary-Layer Interactions at Mach Numbers of 1.3, 1.4 and 1.5,” NASA Tech. Rept. 82099, 1982.

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