Performance, Vibration, Load, and Whirl Flutter Stability Analyses of Tiltrotors with Swept-Back Blades

Author:

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

Funder

National Research Foundation of Korea

Ministry of Science and ICT

Chungnam National University

Publisher

Springer Science and Business Media LLC

Reference35 articles.

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2. Singh P (2023) Flight dynamics and control of the Butterfly eVTOL aircraft in hover. In: Proceedings of the vertical flight society’s 79th annual forum & technology display

3. Brocklehurst A, Barakos GN (2013) A review of helicopter rotor blade tip shapes. Prog Aerosp Sci 56:35–74

4. Mantay WR, Yeager Jr WT (1983) Parametric tip effects for conformable rotor applications. NASA Langley Research Center. AVRADCOM-TR-83-B-4

5. McVeigh MA, McHugh FJ (1984) Influence of tip shape, chord, blade number, and airfoil on advanced rotor performance. J Am Helicopter Soc 29(4):55–62

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