@incollection{, 8487C24363F0C19A970FE24379E0F9BD , author={{Venkatesha BK} and {rashanth KP} and {Deepak KumarT} and {University Visvesvaraya College of Engineering}}, journal={{Global Journal of Researches in Engineering}}, journal={{GJRE}}2249-45960975-586110.34257/gjre, address={Cambridge, United States}, publisher={Global Journals Organisation}1411119 } @incollection{b0, , title={{Fuselage metal fatigue in large commercial aircraft}} , author={{ GeorgeBibel }} , journal={{Int. J. Forensic Engineering}} 1 1 , year={2012} } @incollection{b1, , title={{On Damage Tolerance Design of Fuselage Structure (Longitudinal cracks)}} , author={{ MPir } and { Toor }} , journal={{Engineering Fracture Mechanics}} 24 6 , year={1986} } @book{b2, , title={{Damage Tolerance of Aircraft Panels}} , author={{ PM S TDe Castro } and { SM OTavares } and { VRichter Trummer } and { PF PDe Matos } and { PM G PMoreira } and { LF MSilva }} , year={2010} 18 } @incollection{b3, , title={{The finite element calculations of stress intensity factors using energy techniques}} , author={{ TKHellen }} , booktitle={{2nd International Conference on Structural Mechanics in Reactor Technology}} Berlin , year={1973} , note={Paper G5/3} } @incollection{b4, , title={{A stiffness derivative finite element technique for determination of crack tip stress intensity factors}} , author={{ DMParks }} , journal={{Int. J. 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Mech}} 9 , year={1977} } @book{b7, , title={{Implementation of the Virtual Crack Closure Technique in engineering FE calculations", Finite element analysis and design, Polish Air Force Institute of Technology}} , author={{ AndrzejLeski }} , year={23 rd October, 2006} 43 , address={Poland} } @incollection{b8, , title={{Finite Element Based Computation of Strain Energy Release Rate by Modified Crack Closure Integral}} , author={{ RSethuraman } and { SKMaiti }} , journal={{Engineering Fracture Mechanics}} 30 2 , year={1988} } @incollection{b9, , title={{Crack Arrest Capabilities in Adhesively Bonded Skin and Stiffener}} , author={{ ShamsuzuhaHabeeb } and { KSRaju }} , booktitle={{Proceedings of the 5th Annual GRASP Symposium}} the 5th Annual GRASP Symposium , year={2009} 16 Wichita State University } @incollection{b10, , title={{The propagation of fatigue cracks in test specimens}} , author={{ NEFrost } and { DugdaleDs }} , journal={{J Mech Phys Solids}} 6 , year={1958} } @book{b11, , title={{Crack growth calculations in 7075-T7351 aluminum alloy under various load spectra using an improved crack-1768, Received}} , author={{ JCNewmanJr } and { ABrot } and { MatiasC }} , year={6th May 2005. 14th November 2005. January 2006} , note={received in revised. accepted 4 th} } @incollection{b12, , title={{The Significance of Fatigue Crack Closure}} , author={{ WolfElber }} , booktitle={{Damage Tolerance in Aircraft Structures}} , publisher={American Society for Testing and Materials} , year={1971} 486 } @incollection{b13, , title={{A rational analytic theory of fatigue}} , author={{ PCParis } and { MPGomez } and { AndersonWp }} , journal={{the Trend Eng}} 13 , year={1961} } @book{b14, , title={{The Practical Use of Fracture Mechanics}} , author={{ DavidBroek }} , year={1988} , publisher={Kluwer academic publishers} , address={USA} } @incollection{b15, , title={{Numerical modelling of crack growth profiles in integral skin-stringer panels}} , author={{ MFossati } and { DColombo } and { AManes } and { M } and { Giglio }} , journal={{Engineering Fracture Mechanics}} 78 , year={March, 2011, accepted on 18th March, 2011} } @incollection{b16, , title={{Fail-Safe Design of Integral Metallic Aircraft Structures Reinforced by Bonded Crack Retarders}} , author={{ XZhang } and { Boscolo } and { GFigueroa-Gordon } and { Allegri } and { Irving }} , journal={{Engineering Fracture Mechanics}} 76 10 , year={4 th FEb, 2008} Department of Aerospace Engineering and Materials, Cranfield University Bedfordshire } @incollection{b17, , title={{Design and Modeling of Selective Reinforcements for Integral Aircraft Structures}} , author={{ MarcoBoscolo } and { GiulianoAllegri } and { XiangZhang }} , journal={{The American Institute of Aeronautics and Astronautics Journal}} 46 9 , year={September 2008} } @incollection{b18, , title={{Study on Damage Tolerance Behavior of Integrally Stiffened Panel and Conventional Stiffened Panel}} , author={{ M }} , journal={{World Academy of Science, Engineering and Technology}} 45 , year={2008} } @incollection{b19, , title={{The Dependence of Fatigue Crack Propagation on Strain Energy Release Rate and Crack Opening Displacement}} , author={{ JMBarson }} , booktitle={{Damage Tolerance in Aircraft Structures}} , publisher={American Society for Testing and Materials} , year={1971} 486 } @incollection{b20, , title={{Fatigue Crack Propagation in Stiffened Panels}} , author={{ CPoe }} , booktitle={{Damage Tolerance in Aircraft Structures}} , publisher={American Society for Testing and Materials} , year={1971} 486 }