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Results: 1-25/67
Authors:
ATLURI SN
ZHU T
Citation: Sn. Atluri et T. Zhu, A NEW MESHLESS LOCAL PETROV-GALERKIN (MLPG) APPROACH IN COMPUTATIONALMECHANICS, Computational mechanics, 22(2), 1998, pp. 117-127
Authors:
ZHU T
ZHANG J
ATLURI SN
Citation: T. Zhu et al., A MESHLESS LOCAL BOUNDARY INTEGRAL-EQUATION (LBIE) METHOD FOR SOLVINGNONLINEAR PROBLEMS, Computational mechanics, 22(2), 1998, pp. 174-186
Authors:
PARK JH
ATLURI SN
Citation: Jh. Park et Sn. Atluri, MIXED-MODE FATIGUE GROWTH OF CURVED CRACKS EMANATING FROM FASTENER HOLES IN AIRCRAFT LAP JOINTS, Computational mechanics, 21(6), 1998, pp. 477-482
Authors:
ZHU T
ATLURI SN
Citation: T. Zhu et Sn. Atluri, A MODIFIED COLLOCATION METHOD AND A PENALTY FORMULATION FOR ENFORCINGTHE ESSENTIAL BOUNDARY-CONDITIONS IN THE ELEMENT FREE GALERKIN METHOD, Computational mechanics, 21(3), 1998, pp. 211-222
Authors:
ZHU T
ZHANG JD
ATLURI SN
Citation: T. Zhu et al., A LOCAL BOUNDARY INTEGRAL-EQUATION (LBIE) METHOD IN COMPUTATIONAL MECHANICS, AND A MESHLESS DISCRETIZATION APPROACH, Computational mechanics, 21(3), 1998, pp. 223-235
Authors:
CHOW WT
ATLURI SN
Citation: Wt. Chow et Sn. Atluri, STRESS INTENSITY FACTORS AS THE FRACTURE PARAMETERS FOR DELAMINATION CRACK-GROWTH IN COMPOSITE LAMINATES, Computational mechanics, 21(1), 1998, pp. 1-10
Authors:
OMORI Y
KOBAYASHI AS
OKADA H
ATLURI SN
TAN PW
Citation: Y. Omori et al., T-EPSILON-ASTERISK INTEGRAL AS A CRACK-GROWTH CRITERION, Mechanics of materials, 28(1-4), 1998, pp. 147-154
Authors:
QUADRELLI BM
ATLURI SN
Citation: Bm. Quadrelli et Sn. Atluri, ANALYSIS OF FLEXIBLE MULTIBODY SYSTEMS WITH SPATIAL BEAMS USING MIXEDVARIATIONAL-PRINCIPLES, International journal for numerical methods in engineering, 42(6), 1998, pp. 1071-1090
Authors:
WANG L
CHOW WT
KAWAI H
ATLURI SN
Citation: L. Wang et al., RESIDUAL STRENGTH OF AGING AIRCRAFT WITH MULTIPLE-SITE DAMAGE MULTIPLE ELEMENT DAMAGE/, AIAA journal, 36(5), 1998, pp. 840-847
Authors:
KIM T
ATLURI SN
LOEWY RG
Citation: T. Kim et al., MODELING OF MICROCRACK DAMAGED COMPOSITE PLATES UNDERGOING NONLINEAR BIMODULAR FLUTTER OSCILLATIONS, AIAA journal, 36(4), 1998, pp. 598-606
Authors:
WANG L
CHOW WT
KAWAI H
ATLURI SN
Citation: L. Wang et al., PREDICTIONS OF WIDESPREAD FATIGUE DAMAGE THRESHOLDS IN AGING AIRCRAFT, AIAA journal, 36(3), 1998, pp. 457-464
Authors:
CHOW WT
ATLURI SN
Citation: Wt. Chow et Sn. Atluri, STRESS INTENSITY FACTORS AS THE FRACTURE PARAMETERS FOR DELAMINATION CRACK-GROWTH IN COMPOSITE LAMINATES, Composites. Part B, Engineering, 28(4), 1997, pp. 375-384
Authors:
GAO XL
ATLURI SN
Citation: Xl. Gao et Sn. Atluri, AN ELASTOPLASTIC ANALYTICAL SOLUTION FOR THE SHRINK-FIT PROBLEM WITH A THIN STRAIN-HARDENING HUB AND AN ELASTIC SOLID SHAFT, Mathematics and mechanics of solids, 2(3), 1997, pp. 335-349
Authors:
GAO XL
ATLURI SN
Citation: Xl. Gao et Sn. Atluri, AN EXACT FINITE DEFORMATION ELASTOPLASTIC SOLUTION FOR THE OUTSIDE-INFREE EVERSION PROBLEM OF A TUBE OF ELASTIC LINEAR-HARDENING MATERIAL, IMA journal of applied mathematics, 58(3), 1997, pp. 259-275
Authors:
WANG L
BRUST FW
ATLURI SN
Citation: L. Wang et al., THE ELASTIC-PLASTIC FINITE-ELEMENT ALTERNATING METHOD (EPFEAM) AND THE PREDICTION OF FRACTURE UNDER WFD CONDITIONS IN AIRCRAFT STRUCTURES .3. COMPUTATIONAL PREDICTIONS OF THE NIST MULTIPLE-SITE DAMAGE EXPERIMENTAL RESULTS, Computational mechanics, 20(3), 1997, pp. 199-212
Authors:
WANG L
BRUST FW
ATLURI SN
Citation: L. Wang et al., THE ELASTIC-PLASTIC FINITE-ELEMENT ALTERNATING METHOD (EPFEAM) AND THE PREDICTION OF FRACTURE UNDER WFD CONDITIONS IN AIRCRAFT STRUCTURES .1. EPFEAM THEORY, Computational mechanics, 19(5), 1997, pp. 356-369
Authors:
WANG L
BRUST FW
ATLURI SN
Citation: L. Wang et al., THE ELASTIC-PLASTIC FINITE-ELEMENT ALTERNATING METHOD (EPFEAM) AND THE PREDICTION OF FRACTURE UNDER WFD CONDITIONS IN AIRCRAFT STRUCTURES .2. FRACTURE AND THE T-ASTERISK-INTEGRAL PARAMETER, Computational mechanics, 19(5), 1997, pp. 370-379
Authors:
KIM T
STEADMAN D
HANAGUD SV
ATLURI SN
Citation: T. Kim et al., ON THE FEASIBILITY OF USING THERMAL-GRADIENTS FOR ACTIVE CONTROL OF INTERLAMINAR STRESSES IN LAMINATED COMPOSITES, Journal of composite materials, 31(16), 1997, pp. 1556-1573
Authors:
CHOW WT
ATLURI SN
Citation: Wt. Chow et Sn. Atluri, COMPOSITE PATCH REPAIRS OF METAL STRUCTURES - ADHESIVE NONLINEARITY, THERMAL CYCLING, AND DEBONDING, AIAA journal, 35(9), 1997, pp. 1528-1535
Authors:
BEOM HG
ATLURI SN
Citation: Hg. Beom et Sn. Atluri, NEAR-TIP FIELDS AND INTENSITY FACTORS FOR INTERFACIAL CRACKS IN DISSIMILAR ANISOTROPIC PIEZOELECTRIC MEDIA, International journal of fracture, 75(2), 1996, pp. 163-183
Authors:
NAGANARAYANA BP
ATLURI SN
Citation: Bp. Naganarayana et Sn. Atluri, A COMPUTATIONAL MODEL FOR ANALYZING INTERACTIVE BUCKLING AND DELAMINATION GROWTH IN COMPOSITE STRUCTURES, Sadhana, 21, 1996, pp. 547-575
Authors:
CHOW WT
ATLURI SN
Citation: Wt. Chow et Sn. Atluri, PREDICTION OF POSTBUCKLING STRENGTH OF STIFFENED LAMINATED COMPOSITE PANELS BASED ON THE CRITERION OF MIXED-MODE STRESS INTENSITY FACTORS, Computational mechanics, 18(3), 1996, pp. 215-224
Authors:
CHOW WT
ATLURI SN
Citation: Wt. Chow et Sn. Atluri, FRACTURE AND FATIGUE ANALYSIS OF CURVED OR KINKED CRACKS NEAR FASTENER HOLES, Finite elements in analysis and design, 23(2-4), 1996, pp. 91-100
Authors:
PIPKINS DS
ATLURI SN
Citation: Ds. Pipkins et Sn. Atluri, APPLICATIONS OF THE 3-DIMENSIONAL FINITE-ELEMENT ALTERNATING METHOD, Finite elements in analysis and design, 23(2-4), 1996, pp. 133-153
Authors:
VASUDEVAN S
OKADA H
ATLURI SN
Citation: S. Vasudevan et al., DEVELOPMENT OF A NEW FRAME FINITE-ELEMENT FOR CRASH ANALYSIS, USING AMIXED VARIATIONAL PRINCIPLE AND ROTATIONS AS INDEPENDENT VARIABLES, Finite elements in analysis and design, 23(2-4), 1996, pp. 155-171