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Results: 1-19 |
Results: 19
OPTIMAL-DESIGN OF GENERAL STIFFENED COMPOSITE CIRCULAR-CYLINDERS FOR GLOBAL BUCKLING WITH STRENGTH CONSTRAINTS
Authors: JAUNKY N KNIGHT NF AMBUR DR
Citation: N. Jaunky et al., OPTIMAL-DESIGN OF GENERAL STIFFENED COMPOSITE CIRCULAR-CYLINDERS FOR GLOBAL BUCKLING WITH STRENGTH CONSTRAINTS, Composite structures, 41(3-4), 1998, pp. 243-252
OPTIMAL-DESIGN OF GRID-STIFFENED COMPOSITE PANELS USING GLOBAL AND LOCAL BUCKLING ANALYSES
Authors: JAUNKY N KNIGHT NF AMBUR DR
Citation: N. Jaunky et al., OPTIMAL-DESIGN OF GRID-STIFFENED COMPOSITE PANELS USING GLOBAL AND LOCAL BUCKLING ANALYSES, Journal of aircraft, 35(3), 1998, pp. 478-486
ON A CONSISTENT FIRST-ORDER SHEAR-DEFORMATION THEORY FOR LAMINATED PLATES
Authors: KNIGHT NF QI YQ
Citation: Nf. Knight et Yq. Qi, ON A CONSISTENT FIRST-ORDER SHEAR-DEFORMATION THEORY FOR LAMINATED PLATES, Composites. Part B, Engineering, 28(4), 1997, pp. 397-405
RESTATEMENT OF FIRST-ORDER SHEAR-DEFORMATION THEORY FOR LAMINATED PLATES
Authors: KNIGHT NF QI YQ
Citation: Nf. Knight et Yq. Qi, RESTATEMENT OF FIRST-ORDER SHEAR-DEFORMATION THEORY FOR LAMINATED PLATES, International journal of solids and structures, 34(4), 1997, pp. 481-492
A REFINED FIRST-ORDER SHEAR-DEFORMATION THEORY AND ITS JUSTIFICATION BY PLANE-STRAIN BENDING PROBLEM OF LAMINATED PLATES (VOL 33, PG 49, 1996)
Authors: QI YQ KNIGHT NF
Citation: Yq. Qi et Nf. Knight, A REFINED FIRST-ORDER SHEAR-DEFORMATION THEORY AND ITS JUSTIFICATION BY PLANE-STRAIN BENDING PROBLEM OF LAMINATED PLATES (VOL 33, PG 49, 1996), International journal of solids and structures, 34(4), 1997, pp. 527-527
RAASCH CHALLENGE FOR SHELL ELEMENTS
Authors: KNIGHT NF
Citation: Nf. Knight, RAASCH CHALLENGE FOR SHELL ELEMENTS, AIAA journal, 35(2), 1997, pp. 375-381
STATIC COLLAPSE OF ELASTIC CIRCULAR ARCHES
Authors: KNIGHT NF CARRON WS
Citation: Nf. Knight et Ws. Carron, STATIC COLLAPSE OF ELASTIC CIRCULAR ARCHES, AIAA journal, 35(12), 1997, pp. 1876-1880
FORMULATION OF AN IMPROVED SMEARED STIFFENER THEORY FOR BUCKLING ANALYSIS OF GRID-STIFFENED COMPOSITE PANELS
Authors: JAUNKY N KNIGHT NF AMBUR DR
Citation: N. Jaunky et al., FORMULATION OF AN IMPROVED SMEARED STIFFENER THEORY FOR BUCKLING ANALYSIS OF GRID-STIFFENED COMPOSITE PANELS, Composites. Part B, Engineering, 27(5), 1996, pp. 519-526
NONLINEAR STRUCTURAL RESPONSE USING ADAPTIVE DYNAMIC RELAXATION ON A MASSIVELY PARALLEL-PROCESSING SYSTEM
Authors: OAKLEY DR KNIGHT NF
Citation: Dr. Oakley et Nf. Knight, NONLINEAR STRUCTURAL RESPONSE USING ADAPTIVE DYNAMIC RELAXATION ON A MASSIVELY PARALLEL-PROCESSING SYSTEM, International journal for numerical methods in engineering, 39(2), 1996, pp. 235-259
A REFINED FIRST-ORDER SHEAR-DEFORMATION THEORY AND ITS JUSTIFICATION BY PLANE-STRAIN BENDING PROBLEM OF LAMINATED PLATES
Authors: QI YQ KNIGHT NF
Citation: Yq. Qi et Nf. Knight, A REFINED FIRST-ORDER SHEAR-DEFORMATION THEORY AND ITS JUSTIFICATION BY PLANE-STRAIN BENDING PROBLEM OF LAMINATED PLATES, International journal of solids and structures, 33(1), 1996, pp. 49-64
COMPARISON OF SYMBOLIC AND NUMERICAL-INTEGRATION METHODS FOR AN ASSUMED-STRESS HYBRID SHELL ELEMENT
Authors: RENGARAJAN G KNIGHT NF AMINPOUR MA
Citation: G. Rengarajan et al., COMPARISON OF SYMBOLIC AND NUMERICAL-INTEGRATION METHODS FOR AN ASSUMED-STRESS HYBRID SHELL ELEMENT, Communications in numerical methods in engineering, 11(4), 1995, pp. 307-316
ASSESSMENT OF STRUCTURAL-ANALYSIS TECHNOLOGY FOR STATIC COLLAPSE OF ELASTIC CYLINDRICAL-SHELLS
Authors: KNIGHT NF MACY SC MCCLEARY SL
Citation: Nf. Knight et al., ASSESSMENT OF STRUCTURAL-ANALYSIS TECHNOLOGY FOR STATIC COLLAPSE OF ELASTIC CYLINDRICAL-SHELLS, Finite elements in analysis and design, 18(4), 1995, pp. 403-431
ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .1. FORMULATION
Authors: OAKLEY DR KNIGHT NF
Citation: Dr. Oakley et Nf. Knight, ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .1. FORMULATION, Computer methods in applied mechanics and engineering, 126(1-2), 1995, pp. 67-89
ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .2. SINGLE-PROCESSOR IMPLEMENTATION
Authors: OAKLEY DR KNIGHT NF
Citation: Dr. Oakley et Nf. Knight, ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .2. SINGLE-PROCESSOR IMPLEMENTATION, Computer methods in applied mechanics and engineering, 126(1-2), 1995, pp. 91-109
ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .3. PARALLEL IMPLEMENTATION
Authors: OAKLEY DR KNIGHT NF WARNER DD
Citation: Dr. Oakley et al., ADAPTIVE DYNAMIC RELAXATION ALGORITHM FOR NONLINEAR HYPERELASTIC STRUCTURES .3. PARALLEL IMPLEMENTATION, Computer methods in applied mechanics and engineering, 126(1-2), 1995, pp. 111-129
IMPROVED ASSUMED-STRESS HYBRID SHELL ELEMENT WITH DRILLING DEGREES OFFREEDOM FOR LINEAR STRESS, BUCKLING AND FREE-VIBRATION ANALYSES
Authors: RENGARAJAN G AMINPOUR MA KNIGHT NF
Citation: G. Rengarajan et al., IMPROVED ASSUMED-STRESS HYBRID SHELL ELEMENT WITH DRILLING DEGREES OFFREEDOM FOR LINEAR STRESS, BUCKLING AND FREE-VIBRATION ANALYSES, International journal for numerical methods in engineering, 38(11), 1995, pp. 1917-1943
BUCKLING OF ARBITRARY QUADRILATERAL ANISOTROPIC PLATES
Authors: JAUNKY N KNIGHT NF AMBUR DR
Citation: N. Jaunky et al., BUCKLING OF ARBITRARY QUADRILATERAL ANISOTROPIC PLATES, AIAA journal, 33(5), 1995, pp. 938-944
BUCKLING ANALYSIS OF GENERAL TRIANGULAR ANISOTROPIC PLATES USING POLYNOMIALS
Authors: JAUNKY N KNIGHT NF
Citation: N. Jaunky et Nf. Knight, BUCKLING ANALYSIS OF GENERAL TRIANGULAR ANISOTROPIC PLATES USING POLYNOMIALS, AIAA journal, 33(12), 1995, pp. 2414-2417
FACTORS INFLUENCING NONLINEAR STATIC RESPONSE PREDICTION AND TEST-ANALYSIS CORRELATION FOR COMPOSITE PANELS
Authors: KNIGHT NF
Citation: Nf. Knight, FACTORS INFLUENCING NONLINEAR STATIC RESPONSE PREDICTION AND TEST-ANALYSIS CORRELATION FOR COMPOSITE PANELS, Composite structures, 29(1), 1994, pp. 13-25
Risultati: 1-19 |