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Chaotic Response of an Airfoil due to Aeroelastic Coupling and Dynamic Stall

Publication Type : Journal Article

Publisher : Aiaa Journal - AIAA J

Source : Aiaa Journal - AIAA J, Volume 45, Issue 1, p.271-280 (2007)

Url : https://www.researchgate.net/publication/245426182_Chaotic_Response_of_an_Airfoil_due_to_Aeroelastic_Coupling_and_Dynamic_Stall

Campus : Coimbatore

School : Department of Aerospace Engineering, School of Engineering

Department : Aerospace

Year : 2007

Abstract : of helicopters indicate that vibratory levels in the fuselage exhibit a wide sprectrum of frequencies, including a few below the rotor revolutions per minute.

Cite this Research Publication : Dr. Laxman Vaitla and Venkatesan, C., “Chaotic Response of an Airfoil due to Aeroelastic Coupling and Dynamic Stall”, Aiaa Journal - AIAA J, vol. 45, no. 1, pp. 271-280, 2007.

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