Transient Aeroelastic Response Control of Shipboard Rotors During Engagements by Gurney Flaps-Reference-Cited by-同舟云学术

Transient Aeroelastic Response Control of Shipboard Rotors During Engagements by Gurney Flaps

Published:2019-03 Issue:2 Volume:56 Page:837-841
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Han Dong¹,Yu Lei¹,Barakos George N.²

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

2. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

Funder

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035282

Reference13 articles.

1. Aeroelastic Analysis of Transient Blade Dynamics During Shipboard Engage/Disengage Operations

2. KellerJ. A. “Analysis and Control of the Transient Aeroelastic Response of Rotors During Shipboard Engagement and Disengagement Operations,” Ph.D. Thesis, Penn State Univ., State College, PA, 2001.

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

4. Analysis of Rotor Start-Up and Shutdown on a Sea-Based Oil Rig

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