Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel-Reference-Cited by-同舟云学术

Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel

Published:2017-07 Issue:4 Volume:54 Page:871-882
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Meritt Ryan J.¹,Schetz Joseph A.²,Marineau Eric C.³,Lewis Daniel R.³,Daniel Derick T.⁴

Affiliation:

1. Ahmic Aerospace LLC, Dayton, Ohio 45440

2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

3. Arnold Engineering Development Complex White Oak, Silver Spring, Maryland 20903

4. Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee 37389

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33657

Reference23 articles.

1. Direct Measurement of Skin Friction in Complex Flows

2. MerittR. J. “Skin Friction Sensor Design Methodology and Validation for High-Speed, High-Enthalpy Flow Applications,” Ph.D. Dissertation, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, 2013.

3. The AEDC Hypervelocity Wind Tunnel 9

4. Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited)

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