Publication Type:

Conference Proceedings

Source:

3rd International Basic Research Conference on Rotorcraft Technology, China (2009)

Cite this Research Publication

V. Laxman, H, B. Y., and C., V., “Effect of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System in Hover and Forward Flight”, 3rd International Basic Research Conference on Rotorcraft Technology. China, 2009.

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