Optimal design of aircraft structures with damage tolerance requirements

Author:

Arrieta A.J.,Striz A.G.

Publisher

Springer Science and Business Media LLC

Subject

Control and Optimization,Computer Graphics and Computer-Aided Design,Computer Science Applications,Control and Systems Engineering,Software

Reference11 articles.

1. Arrieta AJ, Striz A (2001) Multidisciplinary design optimization of a fighter aircraft with damage tolerance constraints and a probabilistic model of the fatigue environment. Doctoral dissertation, University of Oklahoma, Norman

2. Broek D (1989) The practical use of fracture mechanics. Kluwer Academic, Boston

3. Chaperon P, Sawyer JP, Jones R (1999) Efficient computational methodology for damage tolerance assessments in conjunction with structural optimisation: phase II, interim report (COE-SM 97-P04), Monash University, Victoria, Australia

4. Curtis H (1997) Fundamentals of aircraft structural analysis. Irwin, Chicago, pp 150–152

5. Damage tolerant design handbook (MCIC HB-01). n.d. Material & Ceramics Info Center, Columbus, OH

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