Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. German-Dutch Wind Tunnels, 38108 Brunswick, Germany
3. DLR, German Aerospace Center, 38108 Brunswick, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031501
Reference21 articles.
1. An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161
2. Prediction of the Flow around the X-31 Aircraft using two different CFD methods
3. Reduced Order Modeling of X-31 Wind Tunnel Model Aerodynamic Loads
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