Back close

Effect of Blade Geometric Parameters on Aeroelastic Response of a Helicopter Rotor System in Hover and Forward Flight

Publication Type : Conference Proceedings

Publisher : 3rd International Basic Research Conference on Rotorcraft Technology

Source : 3rd International Basic Research Conference on Rotorcraft Technology. China, 2009.

Campus : Coimbatore

School : Department of Aerospace Engineering, School of Engineering

Department : Aerospace

Year : 2009

Abstract :

Cite this Research Publication : Dr. Laxman Vaitla, Byun Y. H., Venkatesan C., “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.

Admissions Apply Now