Technical Notes: Minimum Weight Design of Helicopter Rotor Blades with Frequency Constraints-Reference-Cited by-同舟云学术

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Technical Notes: Minimum Weight Design of Helicopter Rotor Blades with Frequency Constraints

Published:1989-10-01 Issue:4 Volume:34 Page:77-82
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Chattopadhyay Aditi¹,Walsh Joanne L.¹

Affiliation:

1. Hampton, Va.

Publisher

American Helicopter Society

Cited by 8 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. Elastic-Dynamic Rotor Blade Design with Multiobjective Optimization;AIAA Journal;2001-09

2. Structural optimization for light-weight articulated rotor blade;41st Structures, Structural Dynamics, and Materials Conference and Exhibit;2000-04-03

3. Design and analysis trends of helicopter rotor systems;Sadhana;1994-06

4. A multidisciplinary optimization approach for vibration reduction in helicopter rotor blades;Computers & Mathematics with Applications;1993-01

5. Optimization of rotor blades for combined structural, dynamic, and aerodynamic properties;Structural Optimization;1992-03

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