Evaluation of vibration reduction devices for helicopter ride quality improvement-Reference-Cited by-同舟云学术

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Evaluation of vibration reduction devices for helicopter ride quality improvement

Published:2019-12 Issue: Volume:95 Page:105456
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Tamer Aykut,Muscarello Vincenzo^ORCID,Masarati Pierangelo^ORCID,Quaranta Giuseppe^ORCID

Funder

Leonardo Helicopter Division

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Whole body vibration exposure for MH-60s pilots;Harrer,2005

2. Modeling aerodynamically generated sound of helicopter rotors;Brentner;Prog. Aerosp. Sci.,2003

3. Rotary Wing Structural Dynamics and Aeroelasticity;Bielawa,2005

4. A closer look at the impact of helicopter vibrations on ride quality;Rath,2017

5. Rotorcraft Aeromechanics;Johnson,2013

Cited by 22 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 isolation by relative resonance perceived in combination of rigid bodies and elastic beams;Journal of Sound and Vibration;2024-05

2. Design optimization of a hexapod vibration isolation system for electro-optical payload;Chinese Journal of Aeronautics;2024-02

3. Development of a High-Performance Low-Weight Hydraulic Damper for Active Vibration Control of the Main Rotor on Helicopters—Part 2: Preliminary Experimental Validation;Aerospace;2023-10-05

4. A Mathematical Model for Dynamic Vibration Analysis of a Landing Aircraft;Journal of Vibration Engineering & Technologies;2023-08-29

5. A low weight electro-hydraulic active damper to control main rotor vibrations on helicopters;2023 3rd International Conference on Electrical, Computer, Communications and Mechatronics Engineering (ICECCME);2023-07-19

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