Active Control of Performance and Vibratory Loads Using Leading Edge Slats

Author:

Ravichandran Kumar,Chopra Inderjit

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. 1Yeo, H. "Assessment of Active Controls for Performance Enhancement," Proceedings of the 62nd Annual Forum of the American Helicopter Society, Phoenix, AZ, 2006.

2. 3Noonan, K. W., Yeager, Jr., W. T., Singleton, J. D., Wilbur, M. L., and Mirick, P. H. "Evaluation of Model Helicopter Main Rotor Blade with Slotted Airfoils at the Tip," Proceedings of the 55th Annual Forum of the American Helicopter Society, Montreal, Canada, May25-27,1999.

3. 4Narramore, J. C., McCroskey, W. J., and Noonan, K. W. "Design and Evaluation of Multi-Element Airfoils for Rotorcraft," Proceedings of the 55th Annual Forum of the American Helicopter Society, Montreal, Canada, May25-27,1999, pp.1960-1970.

4. 5Yeo, H., andLim, J.W. "ApplicationofaSlottedAirfoilforUH-60AHelicopterPerformance," ProceedingsofTheAmerican Helicopter Society Aerodynamics, Aeroacoustics, and Test and Evaluation Technical Specialists Meeting, San Francisco, CA, January23-252002.

5. 6Lorber, P. F., Bagai, A., and Wake, B. E. "Design and Evaluation of Slatted Airfoils for Improved Rotor Performance," 62nd Annual Forum and Technology Display of the American Helicopter Society International, Phoenix, AZ, May9-112006.

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