A study of feedback, blade and hub parameters on flap bending due to non-uniform rotor disk turbulence-Reference-Cited by-同舟云学术

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A study of feedback, blade and hub parameters on flap bending due to non-uniform rotor disk turbulence

Published:1977-04 Issue:4 Volume:51 Page:501-515
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Gaonkar G.H.,Subramanian A.K.

Publisher

Elsevier BV

Subject

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

Reference22 articles.

1. Flapping response of lifting rotor blades to atmospheric turbulence;Gaonkar;Journal of Aircraft,1969

2. Stochastic properties of turbulence existed-rotor blade vibrations;Gaonkar;American Institute of Aeronautics and Astronautics Journal,1971

3. Flying qualities of piloted V/STOL aircraft;Military Specification;MIL-F-83300,1970

4. Helicopter flying and ground handling qualities;Military Specification;MIL-H-8501A (Amendment),1962

5. Research on helicopter rotors;Hohenemser,1969

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Gust Response of Rotor and Propeller Systems;Journal of Aircraft;1981-05

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