The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance-Reference-Cited by-同舟云学术

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The Mach 6 Quiet Tunnel at Texas A&M: Quiet Flow Performance

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
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Author:

Hofferth Jerrod¹,Bowersox Rodney¹,Saric William¹

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4794

Reference9 articles.

1. NASA Langley Mach 6 Quiet Wind-Tunnel Performance

2. Goertler instability and hypersonic quiet nozzle design

3. MackLM. 1984 AGARD Rep.No. 709,VonKarman Inst., Rhode-St.Genese, Belg.

4. Reshotko E. 2007.Is Re /Meameaningfultransitioncriterion?AIAAJ.45(7):1441-3.

5. Görtler Vortices

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1. Development and characterization of high Mach nozzle using high-frequency optical and surface techniques;AIAA SCITECH 2024 Forum;2024-01-04

2. Optical Measurements of Nonlinear Mack Mode Interactions on a Cooled Flared Cone in Quiet Mach 6 Flow;AIAA SCITECH 2024 Forum;2024-01-04

3. Görtler Instability and Transition in Compressible Flows;AIAA Journal;2023-12-29

4. Design and Initial Characterization of the UTSI Mach 7 Ludwieg Tube;AIAA SCITECH 2023 Forum;2023-01-19

5. Measurement of Wall-Cooling Effects on Hypersonic Boundary-Layer Transition Using Focused Laser Differential Interferometry;AIAA Journal;2022-11

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