Viscous interaction effects on a static pressure probe at m equals 6-Reference-Cited by-同舟云学术

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Viscous interaction effects on a static pressure probe at m equals 6

Published:1963-12 Issue:12 Volume:1 Page:2864-2866
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

BEHRENS WILHELM¹

Affiliation:

1. California Institute of Technology, Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.2193

Reference7 articles.

Cited by 20 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. High-Frequency Static Pressure Measurements in the T5 Reflected Shock Tunnel;AIAA SCITECH 2024 Forum;2024-01-04

2. Renewed characterization of a Mach 6 hypersonic wind tunnel;AIAA SCITECH 2023 Forum;2023-01-19

3. Freestream Static Pressure Measurements in the T5 Reflected Shock Tunnel;AIAA SCITECH 2022 Forum;2022-01-03

4. Free-stream static pressure measurements in the Longshot hypersonic wind tunnel and sensitivity analysis;Experiments in Fluids;2016-04-16

5. Design of Static Pressure Probes for Improved Free-Stream Characterization in Hypersonic Wind-Tunnels;52nd Aerospace Sciences Meeting;2014-01-10

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