Dynamic Loads in the Fan Containment Structure of a Turbofan Engine-Reference-Cited by-同舟云学术

Dynamic Loads in the Fan Containment Structure of a Turbofan Engine

Published:2009-07 Issue:3 Volume:22 Page:260-269
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Sinha Sunil K.¹²,Dorbala Sreekanth¹²

Affiliation:

1. Principal Engineer, Non-linear Dynamics, GE Aviation, Cincinnati, OH 45215 (corresponding author).

2. Lead Engineer, Bangalore Engineering Center, GE India—JFWTC, Bangalore 560066, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282009%2922%3A3%28260%29

Reference33 articles.

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2. Australian Transport Safety Bureau Canberra ACT. (2002). “Examination of a failed Rolls-Royce RB211-524 turbofan engine—Boeing Commercial Aircraft Group 747-436 G-BNLD.” Technical Analysis Rep. No. 20/02 Occurrence File No. BO/200200646 Australian Transport Safety Bureau Canberra Australia.

3. Rub in high performance turbomachinery, modeling, solution methodology and signature analysis

4. Cosme N. Chevrolet D. Bonini J. Peseux B. and Cartraud P. (2002). “Prediction of engine loads and damages due to blade-off event.” Proc. 43rd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. Denver American Institute of Aeronautics and Astronautics Reston Va.

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