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G. Thomann (1956)
Aeroelastic Problems of Low Aspect Ratio WingsAircraft Engineering and Aerospace Technology, 28
J. Heyman (1967)
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The upper bound theorem for rigid/plastic solids generalized to include Coulomb frictionJournal of The Mechanics and Physics of Solids, 17
In this paper a technique previously developed for the analysis of rigid‐plastic structural frames is adapted to provide a formal procedure for finding the limit load of any structure formed from rigid blocks. In this procedure the load factor is maximized subject to the euilibrium equations of the structure and linear constraints imposed by criteria of failure at the block interfaces.
International Journal for Numerical Methods in Engineering – Wiley
Published: Jan 1, 1978
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