Interrelated effects of pitch rate and pivot point on airfoil dynamic stall-Reference-Cited by-同舟云学术

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Interrelated effects of pitch rate and pivot point on airfoil dynamic stall

Published:1985-01-14 Issue: Volume: Page:
ISSN:
Container-title:23rd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

HELIN H.¹,WALKER J.²

Affiliation:

1. U.S. Air Force Academy; USAF, Frank J. Seiler ResearchLaboratory, Colorado Springs, CO

2. USAF, Frank J. Seiler Research Laboratory, Colorado Springs, CO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-130

Cited by 16 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Repeatability of Dynamic Stall at Low Reynolds Number;AIAA SCITECH 2024 Forum;2024-01-04

2. Dynamic stall at high Reynolds numbers induced by ramp-type pitching motions;Journal of Fluid Mechanics;2022-03-14

3. Effects of Pivot Location and Reduced Pitch Rate on Pitching Rectangular Flat Plates;AIAA Journal;2017-03

4. Effects of Planform Geometry and Pivot Axis Location on the Aerodynamics of Pitching Low Aspect Ratio Wings;43rd Fluid Dynamics Conference;2013-06-22

5. Visualization and PIV study of wing-tip vortices for three different tip configurations;Aerospace Science and Technology;2012-01

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