Reducing the effects of rivet holes on fatigue life by adhesive bonding-Reference-Cited by-同舟云学术

Reducing the effects of rivet holes on fatigue life by adhesive bonding

Published:1985-05 Issue:2 Volume:3 Page:113-124
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Mann J.Y.,Pell R.A.,Jones R.,Heller M.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference10 articles.

1. Extending the fatigue life of a fighter aircraft wing;Mann,1981

2. Improving the fatigue life of the Mirage III0 wing main spar;Mann;Dept. Defence, Aero. Res. Labs, Structures Report 398,1984

3. Improving the fatigue performance of thick aluminium alloy bolted joints by cold-expansion and the use of interference-fit steel bushes;Mann;Dept. Defence, Aero. Res. Labs, Structures Note 486,1983

4. New thoughts on stopping cracks which emanate from holes;Jones;Int. Jnl. Fracture,1981

5. Fatigue of Welded Structures;Gurney,1979

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