Experimental and Numerical Study to Predict Residual Growth in an Aeroengine Compressor Disc After Overspeed-Reference-Cited by-同舟云学术

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Experimental and Numerical Study to Predict Residual Growth in an Aeroengine Compressor Disc After Overspeed

Published:2013 Issue: Volume:55 Page:625-630
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Ayyappan C.,Kumar Rajesh,Ramesh P.,Jain Rajeev

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference16 articles.

1. Mil-HDBK-5H, Military Handbook, Department of Defence, USA. (1998).

2. M.H. Lee Wu, NACA Report No 1021, (1951).

3. A. Nadai, and L.H. Donnell, Transactions, ASME, APM-51-61(1929).

4. U. Güven, International Journal of Mechanical Sciences, 34 (1992) 133.

5. E.M. Harman and M.D. Rauses, Report No R78AEG096, General Electric Company Lynn, MA 01910 (1978).

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2. Stresses and Deformation in Rotating Disk During Over-Speed;Lecture Notes on Multidisciplinary Industrial Engineering;2019

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