Ganguli, Ranjan (2017) Rotor Blade Finite Element. [Book Chapter]
Full text not available from this repository.Abstract
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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