Identification of Experimental Unsteady Aerodynamic Impulse Responses
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.13151
Reference14 articles.
1. Experimental steady and unsteady aerodynamic and flutter results for HSCT semispan models
2. A new forced oscillation capability for the Transonic Dynamics Tunnel
3. Measurement of Unsteady Pressure Data on a Large HSCT Semispan Wing and Comparison with Analysis
4. AVIA - Adaptive virtual aerosurface
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