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NASA NTRS · 19670035237

Optimum design - Minimum weight versus fully stressed.

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Abstract

Lagrange multiplier matrix in minimum weight and fully stressed optimum structural design techniques

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OPTIMIZATION STRESS ANALYSIS FAILURE MODE LAGRANGE MULTIPLIER WEIGHT ANALYSIS STRUCTURAL DESIGN

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Kicher, T. P.. 1966-12-01. Optimum design - Minimum weight versus fully stressed.. https://ntrs.nasa.gov/citations/19670035237

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