Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap-Reference-Cited by-同舟云学术

Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Chandrasekhara Muguru¹,Martin Preston²,Tung Chee²

Affiliation:

1. Naval Postgraduate School

2. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-41

Reference7 articles.

1. Prouty, R.W. "Aerodynamic: The Gurney Flap, Part1,"AviationToday,Rotor&Wing,Feb.2000.

2. Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing

3. Fuglsang, P., Bak, C., Gaunaa, M., and Antoniou, I. "Wind Tunnel Tests of Riso-B1-18 and Riso-B1-24," Risoe National Laboratory Report Riso-R1375(EN),Roskilde,Denmark, Jan.2003.

Cited by 12 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. Trailing Edge Flap Effects on Dynamic Stall Vortex and Unsteady Aerodynamic Forces on a Pitching Airfoil;International Journal of Aerospace Engineering;2022-03-12

2. Combined Numerical and Experimental Study on the Use of Gurney Flaps for the Performance Enhancement of NACA0021 Airfoil in Static and Dynamic Conditions;Journal of Engineering for Gas Turbines and Power;2021-01-13

3. Effect of Gurney Flap Geometry on a S809 Airfoil;International Journal of Aerospace Engineering;2019-07-18

4. Coupled Aeroelastic Prediction of the Effects of Leading-Edge Slat on Rotor Performance;Journal of Aircraft;2016-01

5. Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows;Journal of Aircraft;2012-05