Individual stress determination in irregularly perforated unsymmetrically-loaded structures from temperature data

Author:

Samad W.A.,Rowlands R.E.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Topology optimization in aircraft and aerospace structures design;Zhu;Arch. Comput. Methods Eng.,2015

2. Optimal topology of aircraft rib and spar structures under aeroelastic loads;Stanford;J. Aircr.,2015

3. Thermoelastic stress analysis of orthotropic composites;Lin;Exp. Mech.,1995

4. Infrared stress analysis of an unsymmetrically-loaded perforated member;Lin,2012

5. Full-field thermoelastic stress analysis of an unsymmetrically-loaded elliptically-perforated structure;Samad,2013

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