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Rotor Blade Finite Element

Ganguli, Ranjan (2017) Rotor Blade Finite Element. [Book Chapter]

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Official URL: https://doi.org/10.1007/978-981-10-1902-9_7


Previous chapters have focused on rotating beams with only the out-of-plane motion. In this chapter, we study rotating blades which have in-plane bending, torsion and axial degrees of freedom. Rotor blades are essential and critical components of helicopters, turbines, compressors and other rotatory machinery (Xiong and Yu, J Sound Vib 302(4–5):821–840, 2007 [1], Thakkar and Ganguli, J Sound Vib 270(4–5):729–753, 2004 [2], Hwang and Kim, J Sound Vib 270(1–2):1–14, 2004 [3], Yoo et al. J Sound Vib 302(4–5):789–805, 2007 [4], Das et al. J Sound Vib 301(1–2):165–188, 2007 [5], Choi et al. J Sound Vib 300(1–2):176–196, 2007 [6]). Blade failure is a severe accident causing the entire machine to shut down.

Item Type: Book Chapter
Series.: Foundations of Engineering Mechanics
Publisher: Springer New York LLC
Additional Information: The Copyright of this article belongs to the Springer
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering)
Date Deposited: 30 May 2022 05:15
Last Modified: 30 May 2022 11:16
URI: https://eprints.iisc.ac.in/id/eprint/72625

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