A multidisciplinary optimization approach for vibration reduction in helicopter rotor blades-Reference-Cited by-同舟云学术

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A multidisciplinary optimization approach for vibration reduction in helicopter rotor blades

Published:1993-01 Issue:2 Volume:25 Page:59-72
ISSN:0898-1221
Container-title:Computers & Mathematics with Applications
language:en
Short-container-title:Computers & Mathematics with Applications

Author:

Chattopadhyay Aditi,McCarthy Thomas R.

Publisher

Elsevier BV

Subject

Computational Mathematics,Computational Theory and Mathematics,Modeling and Simulation

Reference22 articles.

1. Recent experiences in multidicipplinary analysis and optimization,1984

2. Application of modern structuraal optimization to vibration reduction in rotorcraft;Friedmann;Vertice,1985

3. Application of numerical optimization methods to helicopter design problems—A survey;Miura;Vertica,1985

4. Helicopter vibration reduction by rotor blade modal shaping;Taylor,1982

5. Design of helicopter rotor blades for optimum dynamic characteristics;Peters;Computers & Mathematics with Applications,1986

Cited by 18 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. Vibration Reduction In Helicopter Rotor With Dynamic Stress Constraints Using Response Surface Methods;Journal of Aerospace Sciences and Technologies;2023-08-13

2. Optimal Sizing of Trailing Edge Flaps for Helicopter Vibration Reduction: A Response Surface Approach;Journal of Aerospace Sciences and Technologies;2023-08-01

3. Response and EPSD of rotor-blade nonlinear system with non-stationary non-Gaussian stochastic excitation via PGHW method;Computers & Mathematics with Applications;2023-07

4. Simulation and Optimization of Control of Selected Phases of Gyroplane Flight;Computation;2018-02-06

5. Introduction;Smart Helicopter Rotors;2015-12-16

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