Comparison of Tiltrotor Whirl Flutter Analyses with Gimballed and Hingeless Hub Models

Author:

Hwang Ui-Jin,Park Jae-SangORCID,Lee Myeong-Kyu

Funder

National Research Foundation of Korea

Ministry of Science and ICT

Publisher

Springer Science and Business Media LLC

Reference19 articles.

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2. Johnson W, Lau BH, Bowles JV (1986) Calculated performance, stability and maneuverability of high-speed tilting-prop-rotor aircraft. NASA-TM-88349

3. Taylor ES, Browne KA (1938) Vibration isolation of aircraft power plants. J Aeronaut Sci 6(2):43–49. https://doi.org/10.2514/8.760

4. Kreshock AR, Acree CW, Kang H, Yeo H (2019) Development of a new aeroelastic tiltrotor wind tunnel testbed. In: AIAA Scitech 2019 Forum

5. Johnson W (1974) Dynamics of tilting proprotor aircraft in cruise flight. NASA-TN-D-7677

Cited by 1 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. Performance, Vibration, Load, and Whirl Flutter Stability Analyses of Tiltrotors with Swept-Back Blades;International Journal of Aeronautical and Space Sciences;2024-09-05

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