Variable Camber Compliant Wing - Wind Tunnel Testing
Author:
Affiliation:
1. University of Dayton
2. Sierra Lobo, Inc.
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1051
Reference22 articles.
1. RETRACTED: Flap side edge noise modeling and prediction
2. Predictions of the effect of wing camber and thickness on airfoil self-noise
3. Design, fabrication, and testing of the DARPA/Wright Lab 'smart wing' wind tunnel model
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