Parameter Variation and the Leading-Edge Vortex of a Rotating Flat Plate
Author:
Affiliation:
1. Department of Mechanical and Industrial Engineering, IIHR Hydroscience and Engineering, University of Iowa, Iowa City, Iowa 52242
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052381
Reference53 articles.
1. HimmelskampH. “Profile Investigations on a Rotating Airscrew,” Ph.D. Thesis, Aerodynamische Versuchsanstalt, Göttingen, 1945.
2. Rotational accelerations stabilize leading edge vortices on revolving fly wings
3. Experimental investigation of some aspects of insect-like flapping flight aerodynamics for application to micro air vehicles
4. The Effect of Aspect Ratio on the Three-Dimensional Vortex Formation of Rotating Flat-Plate Wings
5. Vortex Formation and Saturation for Low-Aspect-Ratio Rotating Flat Plates at Low Reynolds Number
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