MHz rate Flow Diagnostics in CUBRC Mach 10 Shock Tunnel-Reference-Cited by-同舟云学术

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MHz rate Flow Diagnostics in CUBRC Mach 10 Shock Tunnel

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Jiang Naibo¹,Hsu Paul¹,Slipchenko Mikhail¹,Roy Sukesh¹,Lauriola Daniel K.²,Webb Austin M.²,Meyer Terrence R.²,Gragston Mark³,Parker Ron⁴,Portoni Phillip⁴,McDemortt Conor⁴,Wadhams Timothy⁴

Affiliation:

1. Spectral Energies LLC

2. Purdue University

3. The University of Tennessee Space Institute

4. CUBRC

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1655

Reference22 articles.

1. Transition and Stability of High-Speed Boundary Layers

2. Transient Growth in Hypersonic Boundary Layers

3. Observations of hypervelocity boundary-layer instability

4. Detection of second-mode instabilities on a flared cone in Mach 6 quiet flow with linear array focused laser differential interferometry

5. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Colinear focused laser differential interferometry and self-aligned focusing schlieren;Applied Optics;2023-06-14

2. Development of a Simple Compact Photodiode Array for Use with Linear Array-FLDI;AIAA SCITECH 2023 Forum;2023-01-19

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