Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps-Reference-Cited by-同舟云学术

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Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps

Published:2003-04-07 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Kim Jun-Sik,Smith Edward,Wang Kon-Well

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1543

Reference25 articles.

1. Lim, J. W., and Chopra, I. "Aeroelastic Optimization of A Helicopter Rotor," Proceedings of the 44th AHS Forum, WashingtonD.C., June 1988.

2. Lim, J. W. "Aeroelastic Optimization of A Helicopter Rotor," Ph.D. Thesis,University of Maryland, College Park, 1988

3. Ganguli, R. "Aeroelastic Optimization of Advanced Geometry and Composite Helicopter Rotors," Ph.D. Thesis,UniversityofMaryland, College Park, 1994.

4. Ganguli, R., and Chopra, I. "Aeroelastic Optimization of An Advanced Geometry Composite Helicopter Rotor," Proceedings of the 51st AHS Forum, Fort Worth, TX, May9-11 1995, pp.965-984.

Cited by 3 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. Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap;AIAA Journal;2020-12

2. Flap-wise loads reduction of rotor blades by embedded flap-wise absorbers;The Aeronautical Journal;2016-05-31

3. Computational Study of the Risø-B1-18 Airfoil with a Hinged Flap Providing Variable Trailing Edge Geometry;Wind Engineering;2005-03

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