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NASA NTRS ยท 20120008193

Failure Assessment of Brazed Structures

Abstract

Despite the great advances in analytical methods available to structural engineers, designers of brazed structures have great difficulties in addressing fundamental questions related to the loadcarrying capabilities of brazed assemblies. In this chapter we will review why such common engineering tools as Finite Element Analysis (FEA) as well as many well-established theories (Tresca, von Mises, Highest Principal Stress, etc) don't work well for the brazed joints. This chapter will show how the classic approach of using interaction equations and the less known Coulomb-Mohr failure criterion can be employed to estimate Margins of Safety (MS) in brazed joints.

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BibTeXRIS

Flom, Yuri. 2012-05-01. Failure Assessment of Brazed Structures. https://ntrs.nasa.gov/citations/20120008193

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