Measurement of Plasma Induced Flow Perturbations Affecting a Mach 4.5 Corner Separation Zone-Reference-Cited by-同舟云学术

Measurement of Plasma Induced Flow Perturbations Affecting a Mach 4.5 Corner Separation Zone

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:55th AIAA Aerospace Sciences Meeting
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Author:

Hedlund Brock E.¹,Houpt Alec W.¹,Gordeyev Stanislav¹,Leonov Sergey B.¹

Affiliation:

1. University of Notre Dame

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0154

Reference23 articles.

1. Transient Plasma Impact on Spectra of Flow Disturbances in a Corner Separation Zone at Mach 4.5

2. S.k. Im, L. Wermer, D. Baccarella, Q. Liu, B. McGann and H. Do, "Ramp Separation Response to Laser-Induced Breakdown Disturbed Boundary Layer at M=4.5," AIAA Paper 2016-0616.

3. Boundary Layer Control for Hypersonic Airbreathing Vehicles

4. Effects of Roughness on Hypersonic Boundary-Layer Transition

5. Role of Transient Growth in Roughness-Induced Transition

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