Failure Analysis of Rotorcraft Composite End Plate Structure Under High-Velocity Bird Impact-Reference-Cited by-同舟云学术

Failure Analysis of Rotorcraft Composite End Plate Structure Under High-Velocity Bird Impact

Published:2016-09-02 Issue:5 Volume:16 Page:864-873
ISSN:1547-7029
Container-title:Journal of Failure Analysis and Prevention
language:en
Short-container-title:J Fail. Anal. and Preven.

Author:

Kumar R. Vijaya

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Safety, Risk, Reliability and Quality,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/s11668-016-0165-3.pdf

Reference19 articles.

1. Federal Aviation Regulations (FAR), Part 29-Airworthiness Standards: Transport Category Rotorcraft

2. Design and Airworthiness Requirements for Service Aircraft, DEF STAN 00-970 PART 7/2: Rotorcraft, Leaflet 206 and Leaflet 711

3. J.S. Wilbeck, Impact Behaviour of Low Strength Projectiles, Air Force Materials Laboratory, Technical Report AFML-TR-77-134, 1977

4. J.S. Wilbeck, J.L. Rand, The development of a substitute bird model. J. Eng. Power 103, 725 (1981)

5. M. Ugrcic, Application of the hydrodynamic theory and the finite element method in the analysis of bird strike in a flat barrier. Sci. Tech. Rev. 62(3–4), 28–37 (2012)

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