Effects of Pivot Location and Reduced Pitch Rate on Pitching Rectangular Flat Plates
Author:
Affiliation:
1. National Defense University, 33551 Taoyuan, Taiwan, Republic of China
2. University of Michigan, Ann Arbor, Michigan 48109
Funder
Ministry of Science and Technology, Taiwan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055244
Reference47 articles.
1. HarperP. W.FlaniganR. E. “The Effect of Rate of Change of Angle of Attack on the Maximum Lift of a Small Model,” NACA TN 2061, March 1950.
2. Experimental investigation of dynamic stall for a pitching airfoil
3. Airfoil dynamic stall performance with large-amplitude motions
4. Interrelated effects of pitch rate and pivot point on airfoil dynamic stall
5. GrahamG. M. “An Experimental Investigation on an Airfoil Pitching at Moderate to High Rates to Large Angles of Attack,” Ph.D. Dissertation, Mechanical Engineering Dept., Texas Tech Univ., Lubbock, TX, 1985.
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