Fatigue Life Estimation of Typical Fighter Aircraft Main Landing Gear Using Finite Element Analysis-Reference-Cited by-同舟云学术

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Fatigue Life Estimation of Typical Fighter Aircraft Main Landing Gear Using Finite Element Analysis

Published:2017-12-27 Issue: Volume: Page:39-52
ISSN:
Container-title:Advances in Structural Integrity
language:
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Author:

Sivaranjani T.,Pavan Kumar D. V. T. G.,Manjunatha C. M.,Manjuprasad M.

Publisher

Springer Singapore

Link

http://link.springer.com/content/pdf/10.1007/978-981-10-7197-3_4

Reference10 articles.

1. P. Beaudet, M. Roth, in Failure analysis case histories of canadian forces aircraft landing gear components. Landing Gear Loads, AGARD Conference Proceedings, 484 (1990)

2. M. Khondker, A.K.M. Lutful Kabir, A. Younes, Md Shelimuzzaman, S. Islam, in Landing Gear Shock Absorber Design, Concordia University, Summer 2009

3. M. Imran, R.M. Shabbir Ahmed, M. Haneef, Static and dynamic response analysis for landing gear of test air crafts. Int. J. Innovative Res. Sci. Eng. Technol. 3(5) (2014)

4. V.N. Divakaran, G.V.V. Ravi Kumar, P. Srinivasa Rao, Aircraft landing gear design and development, Infosys, 2015

5. Altair HyperMesh software, version 12.0, Altair HyperWorks

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