Aeroelastic analysis of a shipboard helicopter rotor with ship motions during engagement and disengagement operations-Reference-Cited by-同舟云学术

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Aeroelastic analysis of a shipboard helicopter rotor with ship motions during engagement and disengagement operations

Published:2012-01 Issue:1 Volume:16 Page:1-9
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Han Dong,Wang Hao-wen,Gao Zheng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Dynamics of Marine Vehicles;Bhattacharyya,1978

2. Multibody modeling of engage and disengage operations of helicopter rotors;Bottasso;Journal of the American Helicopter Society,2001

3. Aeroelastic analysis of transient blade dynamics during shipboard engage/disengage operations;Geyer;Journal of Aircraft,1998

4. Lagwise loads analysis of a rotor blade with an embedded chordwise absorber;Han;Journal of Aircraft,2008

5. D.H. Hodges, E.H. Dowell, Nonlinear equations of motion for the elastic bending and torsion of twisted non-uniform blades, NASA TN 7818, 1974.

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1. Dynamic modeling and analysis of traction operation process for the shipboard helicopter;Aerospace Science and Technology;2023-11

2. Numerical studies on the aeroelasticity of a shipboard helicopter rotor during engagement and disengagement with ship motions using CFD/CSD coupling approach;Aerospace Science and Technology;2023-10

3. Transient Aeroelastic Response of a Rotor During Rotor Speed Transition in Forward Flight;Journal of Aircraft;2022-07

4. Insight into the factors affecting the safety of take-off and landing of the ship-borne helicopter;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-11-03

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