Three-dimensional nonlinear finite element analysis of dovetail joints in aeroengine discs
Author:
Publisher
Elsevier BV
Subject
Applied Mathematics,Computer Graphics and Computer-Aided Design,General Engineering,Analysis
Reference13 articles.
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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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