Nonlinear Flexible Multibody Dynamic Analysis of Rotor Blades with a Trailing Edge Flap-Reference-Cited by-同舟云学术

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Nonlinear Flexible Multibody Dynamic Analysis of Rotor Blades with a Trailing Edge Flap

Published:2006-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th
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Author:

Das Manabendra,Barut Atila,Madenci Erdogan,Straub Friedrich

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Modeling rotorcraft dynamics with finite element multibody procedures

2. Rotary Wing Aeroelasticity-A Historical Perspective

3. New developments in vibration reduction with actively controlled trailing edge flaps

4. 4Straub, F. K. and Charles, B. D. "Comprehensive Modeling of Rotors with Trailing Edge Flap," Proceedings of the 55thAnnualForum,Vol.1,pp.523-532,AmericanHelicopterSociety,Montreal,Canada,1999.

Cited by 3 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. Multibody Dynamic Approach of Flight Dynamics and Nonlinear Aeroelasticity of Flexible Aircraft;AIAA Journal;2011-01

2. A Refined and Efficient Approach for Dynamic Analysis of Helicopter Blades;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

3. Aeroelastic Analysis of Rotor Blades Using Three Dimensional Flexible Multibody Dynamic Analysis;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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