-
1
-
-
28844501026
-
-
Version 6.1, Hibbitt, Karlsson & Sorensen, Pawtucket, RI
-
ABAQUS User's Manual, Vol. III, Version 6.1, Hibbitt, Karlsson & Sorensen, Pawtucket, RI, 2000.
-
(2000)
ABAQUS User's Manual
, vol.3
-
-
-
3
-
-
0033279903
-
A progressive damage model for mechanically fastened joints in composite laminates
-
Camanho, P.P., and Matthews, F.L., "A Progressive Damage Model for Mechanically Fastened Joints in Composite Laminates," Journal of Composite Materials, Vol. 33, No. 24, 1999, pp. 2248-2280.
-
(1999)
Journal of Composite Materials
, vol.33
, Issue.24
, pp. 2248-2280
-
-
Camanho, P.P.1
Matthews, F.L.2
-
4
-
-
0023420567
-
A progressive damage model for laminated composites containing stress concentrations
-
Chang, F.-K., and Chang, K.Y., "A Progressive Damage Model for Laminated Composites Containing Stress Concentrations," Journal of Composite Materials, Vol. 21, 1987, pp. 834-855.
-
(1987)
Journal of Composite Materials
, vol.21
, pp. 834-855
-
-
Chang, F.-K.1
Chang, K.Y.2
-
5
-
-
0025741967
-
Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part I-analysis
-
Chang, F.-K., and Lessard, L.B., "Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: Part I-Analysis," Journal of Composite Materials, Vol. 25, 1991, pp. 2-43.
-
(1991)
Journal of Composite Materials
, vol.25
, pp. 2-43
-
-
Chang, F.-K.1
Lessard, L.B.2
-
6
-
-
0343442402
-
Analytical prediction of damage growth in notched composite panels loaded in compression
-
Dávila, C.G., Ambur, D.R., and McGowan, D.M., "Analytical Prediction of Damage Growth in Notched Composite Panels Loaded in Compression," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 898-905.
-
(2000)
Journal of Aircraft
, vol.37
, Issue.5
, pp. 898-905
-
-
Dávila, C.G.1
Ambur, D.R.2
McGowan, D.M.3
-
7
-
-
0035000724
-
Mixed-mode decohesion elements for analyses of progressive delamination
-
Structural Dynamics and Materials Conference, Seattle, Washington, April 16-19
-
Dávila, C.G., Camanho, P.P., and de Moura, M.F.S.F., "Mixed-Mode Decohesion Elements for Analyses of Progressive Delamination," Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Seattle, Washington, April 16-19, 2001(a).
-
(2001)
Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC Structures
-
-
Dávila, C.G.1
Camanho, P.P.2
De Moura, M.F.S.F.3
-
8
-
-
0029755059
-
Geometrical and finite element modeling of textile composites
-
Glaessgen, E.H., Pastore, C.M., Griffin, O.H., Jr. and Birger, A., "Geometrical and Finite Element Modeling of Textile Composites," Composites Part B, Vol. 27B, No. 1, 1996, pp. 43-50.
-
(1996)
Composites Part B
, vol.27 B
, Issue.1
, pp. 43-50
-
-
Glaessgen, E.H.1
Pastore, C.M.2
Griffin Jr., O.H.3
Birger, A.4
-
9
-
-
0015673545
-
A fatigue criterion for fiber-reinforced materials
-
Hashin, Z., and Rotem, A., "A Fatigue Criterion for Fiber-Reinforced Materials," Journal of Composite Materials, Vol. 7, 1973, pp. 448-464.
-
(1973)
Journal of Composite Materials
, vol.7
, pp. 448-464
-
-
Hashin, Z.1
Rotem, A.2
-
10
-
-
0019024701
-
Failure criteria for unidirectional fiber composites
-
Hashin, Z., "Failure Criteria for Unidirectional Fiber Composites," J. Appl. Mech., Vol. 47, 1980, pp. 329-334.
-
(1980)
J. Appl. Mech.
, vol.47
, pp. 329-334
-
-
Hashin, Z.1
-
13
-
-
0022861936
-
Survey of failure and post-failure theories of laminated fiber-reinforced composites
-
Nahas., M.N., "Survey of Failure and Post-Failure Theories of Laminated Fiber-Reinforced Composites," J. Composites Technology and Research, Vol. 8, No. 4, 1986, pp. 138-153.
-
(1986)
J. Composites Technology and Research
, vol.8
, Issue.4
, pp. 138-153
-
-
Nahas, M.N.1
-
14
-
-
84867649356
-
Mechanics of textile composites conference
-
October
-
Poe, C.C., Jr. and Harris, C.E., "Mechanics of Textile Composites Conference," NASA CP 3311, Parts 1 and 2, October 1995.
-
(1995)
NASA CP
, vol.3311
, Issue.1-2 PARTS
-
-
Poe Jr., C.C.1
Harris, C.E.2
-
15
-
-
0002367197
-
Strength (failure) theories and their experimental correlation
-
Failure Mechanics of Composites, ed. G.C. Sih and A. M. Skudra. North-Holland
-
Rowlands, R.E., Strength (Failure) Theories and Their Experimental Correlation. In Handbook of Composites, Vol. 3. Failure Mechanics of Composites, ed. G.C. Sih and A. M. Skudra. North-Holland, 1984, pp. 71-125.
-
(1984)
Handbook of Composites
, vol.3
, pp. 71-125
-
-
Rowlands, R.E.1
-
16
-
-
0032125290
-
A comparison of the predictive capabilities of current failure theories for composite laminates
-
Soden, P.D., Hinton, M.J. and Kaddour, A.S., "A Comparison of the Predictive Capabilities of Current Failure Theories for Composite Laminates," Composites Science and Technology, Vol. 58, 1998(a), pp. 1225-1254.
-
(1998)
Composites Science and Technology
, vol.58
, pp. 1225-1254
-
-
Soden, P.D.1
Hinton, M.J.2
Kaddour, A.S.3
-
17
-
-
0032125036
-
Lamina properties, lay-up configurations and loading conditions for a range of fibre-reinforced composite laminates
-
Soden, P.D., Hinton, M.J. and Kaddour, A.S., "Lamina Properties, Lay-Up Configurations and Loading Conditions for a Range of Fibre-Reinforced Composite Laminates," Composites Science and Technology, Vol. 58, 1998(b), pp. 1011-1022.
-
(1998)
Composites Science and Technology
, vol.58
, pp. 1011-1022
-
-
Soden, P.D.1
Hinton, M.J.2
Kaddour, A.S.3
-
18
-
-
28844432075
-
Structural analysis for the American airlines flight 587 accident investigation - Global analysis
-
Structural Dynamics, and Materials Conference, AIAA-2005-2254-CP, AIAA, Austin, TX, April 18-21
-
Young, R.D., Hilberger, M., Moore, D. and Lovejoy, A.E., 'Structural Analysis for the American Airlines Flight 587 Accident Investigation - Global Analysis," Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA-2005-2254-CP, AIAA, Austin, TX, April 18-21, 2005.
-
(2005)
Proceedings of the 46th AIAA/ASME/ASCE/AHS/ASC Structures
-
-
Young, R.D.1
Hilberger, M.2
Moore, D.3
Lovejoy, A.E.4
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