Active Yaw Control with a Wire Suspension System for Dynamic Wind Tunnel Testing
Author:
Affiliation:
1. Physical Sciences Inc.
2. Physical Science, Inc.
3. Naval Air Warfare Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1295
Reference5 articles.
1. Design of a Wire Suspension System for Dynamic Testing in AEDC 16T
2. 2Magill, J. C., Cataldi, P., Morency, J. R., Jeter, E., Burgess, R., and Daugherty, C. "Demonstration of a Wire Suspension Systemfor Dynamic Wind Tunnel Testing", AIAA-2004-1296.
3. 3Ratliff, C. L. and Marquart. E. J. "An Assessment of a Potential Flight Test Technique: Virtual Flight Testing,@ AIAA 95-3472,AIAAAtmosphericFlight Mechanics Conference, August7-9, 1995.
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1. Demonstration of a Wire Suspension for Wind-Tunnel Virtual Flight Testing;Journal of Spacecraft and Rockets;2009-05
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