Publication Type : Journal Article
Publisher : Aerospace Sciences and Technologies
Source : Aerospace Sciences and Technologies, Volume 61, Issue 3, p.415 -433 (2009)
Url : http://home.iitk.ac.in/~shekhar/structure%20lab/Y210166.pdf
Campus : Coimbatore
School : Department of Aerospace Engineering, School of Engineering
Department : Aerospace
Year : 2009
Abstract : Rotary wing aeroelasticity is a highly complex phenomenon involving coupling between flexible blade dynamics, unsteady aerodynamics including stall and unsteady wake effects.
Cite this Research Publication : Dr. Laxman Vaitla and C, V., “Formulation of a Computational Aeroelastic Model to Predict Trim and Response of a Helicopter Rotor System”, Aerospace Sciences and Technologies, vol. 61, no. 3, pp. 415 -433, 2009.