A theoretical analysis of the effect of the modulus of elasticity and other parameters upon the flutter of a helicopter rotor blade in hovering flight.

A theoretical analysis of the effect of the modulus of elasticity and other parameters upon the flutter of a helicopter rotor blade in hovering flight.

Bibliographic Details
Main Author: Swah, Samuel Ryan.
Other Authors: Dept. of Aerospace and Mechanical Sciences
Language:en_US
Published: Princeton University 2012
Online Access:http://hdl.handle.net/10945/9651

Internet

http://hdl.handle.net/10945/9651

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