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