Establishment Times of Hypersonic Shock-Wave/Boundary-Layer Interactions in Intermittent Facilities-Reference-Cited by-同舟云学术

Establishment Times of Hypersonic Shock-Wave/Boundary-Layer Interactions in Intermittent Facilities

Published:2017-09 Issue:9 Volume:55 Page:2875-2887
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Vanstone Leon¹,Estruch-Samper David²,Ganapathisubramani Bharathram³

Affiliation:

1. University of Texas at Austin, Austin, Texas 78724

2. National University of Singapore, Singapore 119077, Republic of Singapore

3. University of Southampton, Southampton, England SO17 1BJ, United Kingdom

Funder

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055575

Reference26 articles.

1. Establishment time of laminar separated flows

2. MEASUREMENTS OF HEAT TRANSFER RATES IN SEPARATED REGIONS IN A SHOCK TUBE AND IN A SHOCK TUNNEL

3. QUASI-STEADY ASPECTS OF THE ADJUSTMENT OF SEPARATED FLOW REGIONS TO TRANSIENT EXTERNAL FLOWS

4. Heat transfer and transition to turbulence in the shock-induced boundary layer on a semi-infinite flat plate

5. GuptaR. N. “An Analysis of the Relaxation of Laminar Boundary Layer on a Flat Plate After Passage of an Interface with Application to Expansion-Tube Flows,” NASA-TR-R-397, L-8514, 1972.

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