Pitch rate and Reynolds number effects on a pitching rectangular wing-Reference-Cited by-同舟云学术

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Pitch rate and Reynolds number effects on a pitching rectangular wing

Published:1988-06-06 Issue: Volume: Page:
ISSN:
Container-title:6th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

ROBINSON MICHAEL¹,WISSLER JOHN²

Affiliation:

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

2. U.S. Air Force Academy, ColoradoSprings, CO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2577

Reference19 articles.

1. 1769-CP, Aug. 1985, pp. 1-33.

2. Experiments," NASA TN-8382. Jan. 1977.

3. Oscillating Airfoils,I' AIAA Paper 75-1 25,

4. Jan. 1975.

5. F_LuLdsJ- 101,1979, pp. 376-330.

Cited by 6 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. An insight into the dynamic stall lift characteristics;Experimental Thermal and Fluid Science;2014-10

2. Pitch Rate and Reynolds Number Effects on Unsteady Boundary-Layer Transition and Separation;Journal of Aircraft;1998-01

3. Surface pressure measurements on a pitching swept wing in a water channel;AIAA Journal;1995-10

4. Measured forces and moments on a delta wing during pitch-up;Journal of Aircraft;1990-03

5. Thrust generation by an airfoil in hover modes;Experiments in Fluids;1990

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