Optimum design of structures with multiple constraints

Automated design of large aerospace structures requires efficient optimization algorithms because of a large number of design variables and design constraints. Most of the difficulties associated with large structural design are solution convergence and computer resources requirements. Practical aer...

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Veröffentlicht in:	AIAA journal 1988-01, Vol.26 (1), p.78-85
Hauptverfasser:	Canfield, R. A, Grandhi, R. V, Venkayya, V. B
Format:	Artikel
Sprache:	eng
Schlagworte:	aerospace engineering computer aided design Exact sciences and technology Fundamental areas of phenomenology (including applications) mathematical programming optimization Physics Solid mechanics Static elasticity (thermoelasticity...) structural analysis Structural and continuum mechanics
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