Analysis of fractured rod assembly of an aircraft

Sujata, M and Bhaumik, SK (2004) Analysis of fractured rod assembly of an aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Full text not available from this repository. (Request a copy)

Abstract

A fractured rod assembly of an aircraft was sent to the laboratory for analysis. The component is made of a number of aluminium alloy tubes joined to each other by welding. Analysis revealed that the tube had fractured at one of the welds by overload. Metallographic examination suggests that inadequate weld joint and weld defects were responsible for the failure.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aircraft;tubes;overload failure;weld defects
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Division/Department: Materials Science Division, Materials Science Division
Depositing User: Mrs Manoranjitha M D
Date Deposited: 29 Jul 2011 11:46
Last Modified: 29 Jul 2011 11:46
URI: http://nal-ir.nal.res.in/id/eprint/9728

Actions (login required)

View Item