Comprehensive Numerical Assessment of Rotorcraft Vibration and Noise Control Using Microflaps
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. The Boeing Company, Mesa, Arizona 85215
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033448
Reference45 articles.
1. Design of Subsonic Airfoils for High Lift
2. Lift enhancement of an airfoil using a Gurney flap and vortex generators
3. Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified Airfoil
4. Experimental Investigation of Gurney Flaps
5. Gurney flap effects and scaling for low-speed airfoils
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