Development of Dynamic Force Measurement Capabilities at AEDC Tunnel 9-Reference-Cited by-同舟云学术

Development of Dynamic Force Measurement Capabilities at AEDC Tunnel 9

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Collopy Arianne¹,Lee Sung¹,Marineau Eric C.²

Affiliation:

1. University of Maryland, College Park

2. Arnold Engineering Development Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0983

Reference13 articles.

1. 1S. J. Laurence, J. M. Schramm, S. Karl, and K. Hannemann, “An Experimental Invesigation of Steady and Unsteady Combustion Phenomenon in the HyShot II Combustor”, AIAA Paper 2011-2310

2. 2M. S. Holden, T. P. Wadhams, J. Harvey, and B. J. Walker, “Experimental and Numerical Studies on Hypersonic Vehicle Performance in the LENS Shock and Expansion Tunnels”, AIAA Paper 2006-125

3. 3S. J. Laurence, H. Ozawa, D. Lieber, J. M. Schramm, and K. Hannemann, “Investigation of Unsteady/Quasi-Steady Scramjet Behavior using High-Speed Visualization Techniques”, AIAA Paper 2012-5913

4. 4L. Resch, C. Decesaris, and E. Hedlund, “The Naval Surface Warfare Center Hypervelocity Wind Tunnel 9 Hypersonic Shroud Testing Capability”, AIAA Paper 92-0676

5. 5L. Resch, L. Zentz, and J. Allwine, “Hypersonic Shroud Separation Testing and Modelling Capabilites at the Naval Surface Warfare Center Hypervelocity Wind Tunnel 9”, AIAA Paper 94-2495

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