Validation of Unsteady Aerodynamic Models of a Generic UCAV Using Overset Grids
Author:
Affiliation:
1. U.S. Air Force Academy
2. University of Southampton
3. Defence Science and Technology Organisation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-2265
Reference45 articles.
1. The NATO STO Task Group AVT-201 on ‘Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles’
2. An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimation: Overview of NATO RTO AVT-161
3. Numerical and experimental analyses of the vortical flow around the SACCON configuration
4. SACCON Static Wind Tunnel Tests at DNW-NWB and 14´x22´ NASA LaRC
5. SACCON Dynamic Wind Tunnel Tests at DNW-NWB and 14´x22´ NASA LaRC
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1. Multi-Disciplinary Design and Performance Assessment of Effective, Agile NATO Air Vehicles;2018 Applied Aerodynamics Conference;2018-06-24
2. Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summary;Journal of Aircraft;2018-03
3. Aerodynamics and Conceptual Design Studies on an Unmanned Combat Aerial Vehicle Configuration;Journal of Aircraft;2018-03
4. The NATO STO Task Group AVT-201 on ‘Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles’;32nd AIAA Applied Aerodynamics Conference;2014-06-13
5. The NATO STO AVT-201 Task Group on Extended assessment of Stability an Control Prediction Methods for NATO Air Vehicles: Summary, Conclusions and Lessons Learned;32nd AIAA Applied Aerodynamics Conference;2014-06-13
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