Fatigue Crack growth study of composite patch repaired Aluminum Al 2014-T6 panel under Variable Amplitude Loading

Pandharkar, Sammed (2015) Fatigue Crack growth study of composite patch repaired Aluminum Al 2014-T6 panel under Variable Amplitude Loading. Masters thesis, Indian Institute of Technology Hyderabad.

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Abstract

In this modern era, use of aircraft in freight, public transport and warfare is increasing day by day. With this increasing demand and ever limited supply, the need of efficient use of already available resources is high. This leads to a need of increasing the lifespan of an aircraft, so it can provide service for longer period of time and ultimately give a relief to from financial stress of replacing the aging aircraft with a new one.

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IITH Creators:	IITH Creators ORCiD
Item Type:	Thesis (Masters)
Uncontrolled Keywords:	FCG, Patch repair, Variable Amplitude Fatigue, FEA, Experimental Analysis, TD468
Subjects:	Others > Mechanics
Divisions:	Department of Physics
Depositing User:	Library Staff
Date Deposited:	04 Aug 2015 11:07
Last Modified:	14 May 2019 09:57
URI:	http://raiithold.iith.ac.in/id/eprint/1781
Publisher URL:
Related URLs:	Google Scholar

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