Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flight-Reference-Cited by-同舟云学术

Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flight

Published:1973-09 Issue:1 Volume:30 Page:9-31
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Friedmann P.,Tong P.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference16 articles.

1. A theory of rotor blade motion stability in powered flight;Young;Journal of the American Helicopter Society,1964

2. A simplified theory of hingeless rotors with application to tandem helicopters;Young;Eighteenth Annual Forum of the American Helicopter Society,1962

3. Aeroelastic instability of torsionally rigid helicopter blades;Hohenemser;Journal of the American Helicopter Society,1967

4. Linear flap-lag dynamics of hingeless helicopter rotor blades in hover;Ormiston;Journal of the American Helicopter Society,1972

5. Aeroelastic instabilities of hingeless helicopter blades;Friedmann;American Institute of Aeronautics and Astronautics 11th Aerospace Sciences Meeting January 1973, AIAA Paper No. 73-193,1973

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