SACCON Dynamic Wind Tunnel Tests at DNW-NWB and 14´x22´ NASA LaRC
Author:
Affiliation:
1. NASA Langley Research Center
2. German-Dutch Wind Tunnels
3. Instituteof Aerodynamics and Flow Technology (DLR)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4394
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1. An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161
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