Unique Testing Capabilities of the NASA Langley Transonic Dynamics Tunnel, an Exercise in Aeroelastic Scaling
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2625
Reference46 articles.
1. Transonic Dynamics Tunnel Aeroelastic Testing in Support of Aircraft Development
2. 3Cole, S. R.; Keller, D. K.; Piatak, D. J. "Contributions of the NASA Langley Transonic Dynamics Tunnel to Launch Vehicleand Spacecraft Development;"AIAA DynamicsSpecialists Conference, Atlanta, GA, April 2000, AIAA2000-1772.
3. 4PerryIII, B. Noll, T. E.; Scott,R. C. "ContributionsoftheTransonic Dynamics Tunnel to theTestingofActiveControlof AeroelasticResponse;" AIAA DynamicSpecialistsConference, Atlanta, GA, April 2000, AIAA2000-1769.
4. Review of CFD Capabilities
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