Three-dimensional nonlinear finite element analysis of dovetail joints in aeroengine discs-Reference-Cited by-同舟云学术

Three-dimensional nonlinear finite element analysis of dovetail joints in aeroengine discs

Published:1998-06 Issue:3-4 Volume:29 Page:173-186
ISSN:0168-874X
Container-title:Finite Elements in Analysis and Design
language:en
Short-container-title:Finite Elements in Analysis and Design

Author:

Papanikos P,Meguid S.A,Stjepanovic Z

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Graphics and Computer-Aided Design,General Engineering,Analysis

Reference13 articles.

1. Theoretical and experimental studies of fretting-initiated fatigue failure of aeroengine compressor discs;Papanikos;Fatigue Fract. Eng. Mater. Struct.,1994

2. Contact stress distributions in a turbine disc dovetail type joint – A comparison of photoelastic and finite element results;Kenny;Strain,1991

3. Experimental determination of stress intensity factors for cracks in turbine discs;Nurse;Fatigue Fract. Eng. Mater. Struct.,1993

4. The numerical analysis of dovetail joints;Boddington;Comput. Struct.,1985

5. V.J. Parks, R.J. Sanford, Experimental stress analysis of the TF-30 turbine engine third-stage fan-blade/disc dovetail region, NRL Report, NRL 8149, August 1977.

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