Impact analysis of compressor rotor blades of an aircraft engine-Reference-Cited by-同舟云学术

Impact analysis of compressor rotor blades of an aircraft engine

Published:2018-09-17 Issue:3 Volume:13 Page:505-514
ISSN:2095-2430
Container-title:Frontiers of Structural and Civil Engineering
language:en
Short-container-title:Front. Struct. Civ. Eng.

Author:

Sudhir Sastry Y B,Kiros B G,Hailu F,Budarapu P R

Publisher

Springer Science and Business Media LLC

Subject

Architecture,Civil and Structural Engineering

Link

http://link.springer.com/content/pdf/10.1007/s11709-018-0493-3.pdf

Reference55 articles.

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2. Biollo R, Benini E. Recent advances in transonic axial compressor aerodynamics. Progress in Aerospace Sciences, 2013, 56: 1–18

3. Boyce M P. Axial-Flow Compressors. 2121 Kirby Drive, Number 28N Houston, TX 77019, 2007

4. Zhang K, Qu W, Wang W. Vibration analysis of an aero-engine compressor blade. In: The Proceeding of 2012 International Conference on Vibration analysis of an aero-engine compressor blade Mechanical Engineering and Material Science, 2012, 85–88

5. Kumar R R. Static structural and modal analysis of gas turbine blade. IOP Conference Series: Materials Science and Engineering, 2017, 225(1): 012102

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