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Damage Tolerance and Durability of the Materials/Structures

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DAMAGE TOLERANCE AND DURABILITY OF THEMATERIALS / STRUCTURESAE 694 – M.Tech SeminarByG.R.R.CharyRoll No 10301404Under <strong>the</strong> guidance <strong>of</strong>Pr<strong>of</strong> N.K.NaikDepartment <strong>of</strong> Aerospace EngineeringIndian Institute <strong>of</strong> Technology, BombayNovember, 2010


References[1] J.B.Ransom Et.al., “Recent Advances in <strong>Durability</strong> <strong>and</strong> <strong>Damage</strong> <strong>Tolerance</strong> Methodologyat NASA Langley Research Center” .[2] Charles.E.Haris et al.,Advanced <strong>Durability</strong> <strong>and</strong> <strong>Damage</strong> <strong>Tolerance</strong> <strong>and</strong> Analysis methodfor Composite Strucutres. NASA / TM – 2003 -212420[3] K.Reifsnider , Scott.W. Case “<strong>Damage</strong> tolerance & durability <strong>of</strong> material systems” Chap1 pp 25 – 43, Chap 3 pp 84 – 85, A John Wiley <strong>and</strong> sons, Inc, 2002[4] H. Razi <strong>and</strong> S. Ward. “Principles for achieving damage tolerant primary compositeaircraft structures”.11th DoD/FAA/NASA Conf. On Fibrous Composites in StructuralDesign, August 1996[5] Jaehyung Ju, Brent D. Pickle, Roger J. Morgan <strong>and</strong> J.N. Reddy. “An Initial <strong>and</strong>Progressive Failure Analysis for Cryogenic Composite Fuel Tank Design” Journal <strong>of</strong>Composite <strong>Materials</strong> 2007, 41: 2545[6] James D Lee., “Three dimensional finite element analysis <strong>of</strong> damage accumulation incomposite laminate”, 1981[7] Tolson S Zabaras N, “Finite element analysis <strong>of</strong> progressive failure in laminatedcomposite plates”. Comput. Str 1991; 38: 361-76[8] Kuen Y. Lin, <strong>and</strong> Andrey V. Stewart, “Probabilistic Approach to <strong>Damage</strong> <strong>Tolerance</strong>Design <strong>of</strong> Aircraft Composite <strong>Structures</strong>,” Journal <strong>of</strong> Aircraft, Vol. 44, No. 4, July–August2007, pp 1309-1317[9] Ushakov, A., Stewart, A., Mishulin, I., <strong>and</strong> Pankov, A., “Probabilistic Design <strong>of</strong><strong>Damage</strong>Tolerant Composite Aircraft <strong>Structures</strong>,” U.S. Department <strong>of</strong> Transportation, FederalAviation Administration, Report DOT/FAA/AR-01/55, Washington, D.C., Jan.2002.[10] H.A. Whitworth. “Evaluation <strong>of</strong> <strong>the</strong> residual strength degradation in compositeLaminates under fatigue loading”. Composite <strong>Structures</strong> 48 (2000) 261-264.[11] Ken Reifsnider etal. “The mechanics <strong>of</strong> composite strength evolution”. CompositesScience <strong>and</strong> Technology 60 (2000) 2539-2546.[12] Mallick P.K.,“Fibre-Reinforced composites materials, Manufacturing & Design”, 2nded. Chapter.4 pp 331 – 340, Marcel Dekker Inc., New York, 1993


[13] O. Ishai, H. Rosenthal, N. Sela, <strong>and</strong> E. Drukker, “Effect <strong>of</strong> selective adhesiveinterleaving on interlaminar fracture toughness <strong>of</strong> graphite epoxy composite laminates”,Composites, 19:49 (1988).[14] C.T. Sun <strong>and</strong> G.D. Chu, “Reducing free edge effect on laminate strength by edgemodification”, J. Compos. Mater., 25:142 (1991).[15] C.T. Sun, “Intelligent tailoring <strong>of</strong> composite laminates”, Carbon, 27:679 (1989).[16] W.S. Chan <strong>and</strong> O.O. Ochoa, “Suppression <strong>of</strong> edge delamination by terminating criticalply near edges in composite laminates”, Key Engineering <strong>Materials</strong> Series,Vol. 37, TranstechPublications, p. 285 (1989).[17] E.W.Y/Lee & W.S.Chan, “Delamination arrestment by discretizing <strong>the</strong> critical ply in alaminate”, AIAA paper no. 89-1403, Amer. Inst. Aero. Asrto., 1898

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