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Failure Assessment of Brazed StructuresDespite 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.
Document ID
20120008193
Acquisition Source
Goddard Space Flight Center
Document Type
Book Chapter
Authors
Flom, Yuri
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2012
Subject Category
Structural Mechanics
Report/Patent Number
GSFC.ABS.5987.2012
Report Number: GSFC.ABS.5987.2012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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