Use of optimization in helicopter vibration control by structural modification-Reference-Cited by-同舟云学术

Use of optimization in helicopter vibration control by structural modification

Published:1981-02 Issue:4 Volume:74 Page:507-518
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Done G.T.S.,Rangacharyulu M.A.V.

Publisher

Elsevier BV

Subject

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

Reference9 articles.

1. Structural optimization under shock and vibration environment;Rao;The Shock and Vibration Digest,1979

2. Structural optimization: a review and some recommendations;Venkayya;International Journal for Numerical Methods in Engineering,1978

3. Use of finite element damped forced response strain energy distribution for vibration reduction;Sciarra;Boeing Vertol Report D210-10819-1,1974

4. A note on the properties of the variation of structural response with respect to a single structural parameter when plotted in the complex plane;Vincent;Westland Helicopters Report GEN/DYN/RES/010R,1973

5. The response of a vibrating structure as a function of structural parameters;Done;Journal of Sound and Vibration,1975

Cited by 4 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. Modeling of Active Vibration Reduction System (AVRS) based on vibration source propagation path;Third International Conference on Mechanical Design and Simulation (MDS 2023);2023-06-16

2. Investigation on the Use of Optimization Techniques for Helicopter Airframe Vibrations Design Studies;Control and Dynamic Systems;1992

3. Optimization of helicopter airframe structures for vibration reduction - Considerations, formulations, and applications;Journal of Aircraft;1991-01

4. Optimization of helicopter airframe structures for vibration reduction considerations, formulations and applications;Aircraft Design, Systems and Operations Conference;1988-08-17