Implication of unequal rivet load distribution in the failures and damage tolerant design of metal and composite civil aircraft riveted lap joints

Author:

Sathiya Naarayan S.,Pavan Kumar D.V.T.G.,Chandra Satish

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference24 articles.

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2. Swift T. Fail-safe requirements and features, regulatory requirements. In: AIAA/CAS international air and space symposium and exposition, the next 100 years, 14–17 July 2003, Dayton, Ohio.

3. Fatigue damage in aircraft structures, not wanted but tolerated;Schijve;Int J Fatigue,2009

4. Safety factors in civil aircraft design requirements;Bristow;Eng Fail Anal,2007

5. Analysis and design of flight vehicle structures;Bruhn,1973

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