ASTM STP23702S PDF

Application of the Hybrid Finite Element Method to Aircraft Repairs

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ASTM STP23702S

Application of the Hybrid Finite Element Method to Aircraft Repairs

Формат:: Электронный (PDF)
SKU:: ASTM STP23702S

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Abstract

A hybrid finite element approach is presented for the analysis of cracked panels with riveted doublers in airframe structures. The method uses the super element developed by Tong to model the cracked panel with rivet holes, springs to model...

ASTM STP23702S PDF

Abstract

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Abstract

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