-
1
-
-
0029753815
-
Delaminations in composite structures: Its origin, buckling, growth and stability
-
Bolotin VV. Delaminations in composite structures: its origin, buckling, growth and stability. Composites: Part B 1996;27:129-45.
-
(1996)
Composites: Part B
, vol.27
, pp. 129-145
-
-
Bolotin, V.V.1
-
3
-
-
85025227928
-
Impact on laminated composite materials
-
Abrate S. Impact on laminated composite materials. Appl Mech Rev 1991;44(4): 155-90.
-
(1991)
Appl Mech Rev
, vol.44
, Issue.4
, pp. 155-190
-
-
Abrate, S.1
-
4
-
-
85025178536
-
Impact on laminated composites: Recent advances
-
Abrate S. Impact on laminated composites: recent advances. Appl Mech Rev 1994;47(11):517-44.
-
(1994)
Appl Mech Rev
, vol.47
, Issue.11
, pp. 517-544
-
-
Abrate, S.1
-
5
-
-
0000323029
-
Static and dynamic response of moderately thick laminated beams with damage
-
Averill RC. Static and dynamic response of moderately thick laminated beams with damage. Compos Eng 1994;4:381-95.
-
(1994)
Compos Eng
, vol.4
, pp. 381-395
-
-
Averill, R.C.1
-
6
-
-
0033309531
-
Effects of interfacial damages on the global and local static response of crossply laminates
-
Di Sciuva M, Icardi U, Librescu L. Effects of interfacial damages on the global and local static response of crossply laminates. Int J Fract 1999;96:17-35.
-
(1999)
Int J Fract
, vol.96
, pp. 17-35
-
-
Di Sciuva, M.1
Icardi, U.2
Librescu, L.3
-
7
-
-
0034825219
-
Unified approach to modeling matrix cracking and delamination in laminated composite structures
-
Thornburgh R, Chattopadhyay A. Unified approach to modeling matrix cracking and delamination in laminated composite structures. AIAA J 2001;39(1):153-60.
-
(2001)
AIAA J
, vol.39
, Issue.1
, pp. 153-160
-
-
Thornburgh, R.1
Chattopadhyay, A.2
-
8
-
-
0031162198
-
A general theory for laminated plates with delaminations
-
Williams TO, Addessio FL. A general theory for laminated plates with delaminations. Int J Solids Struct 1997;34(16):2003-24.
-
(1997)
Int J Solids Struct
, vol.34
, Issue.16
, pp. 2003-2024
-
-
Williams, T.O.1
Addessio, F.L.2
-
9
-
-
0026205953
-
A new approach toward understanding damage mechanism and mechanics of laminated composites due to low velocity impact: Part II-analysis
-
Choi HY, Wu HYT. A new approach toward understanding damage mechanism and mechanics of laminated composites due to low velocity impact: Part II-analysis. J Comput Math 1991;25(8):1012-38.
-
(1991)
J Comput Math
, vol.25
, Issue.8
, pp. 1012-1038
-
-
Choi, H.Y.1
Wu, H.Y.T.2
-
10
-
-
0026998703
-
A model for predicting damage in graphite/epoxy laminated composites resulting from low velocity point impact
-
Choi HY, Chang FK. A model for predicting damage in graphite/epoxy laminated composites resulting from low velocity point impact. J Comput Math 1992;26(14):2134-69.
-
(1992)
J Comput Math
, vol.26
, Issue.14
, pp. 2134-2169
-
-
Choi, H.Y.1
Chang, F.K.2
-
11
-
-
0031136301
-
Damage growth analysis of low velocity impacted composite panels
-
Reis L, de Freitas M. Damage growth analysis of low velocity impacted composite panels. Compos Struct 1997;38(1-4):509-15.
-
(1997)
Compos Struct
, vol.38
, Issue.1-4
, pp. 509-515
-
-
Reis, L.1
De Freitas, M.2
-
12
-
-
0033727498
-
Numerical evaluation of failure mechanism on composite specimens subjected to impact loading
-
de Freitas M, Numerical evaluation of failure mechanism on composite specimens subjected to impact loading. Composites: Part B 2000;31:199-207.
-
(2000)
Composites: Part B
, vol.31
, pp. 199-207
-
-
De Freitas, M.1
-
13
-
-
0032125290
-
A comparison of the predictive capabilities of current failure theories for composite laminates
-
Soden PD, Hinton MJ, Kaddour AS. A comparison of the predictive capabilities of current failure theories for composite laminates. Comput Sci Technol 1998;58:1225-54.
-
(1998)
Comput Sci Technol
, vol.58
, pp. 1225-1254
-
-
Soden, P.D.1
Hinton, M.J.2
Kaddour, A.S.3
-
14
-
-
26144449748
-
Impact damage simulation and compression after impact of composite stiffened panels
-
Chai Y, Gädke M. Impact damage simulation and compression after impact of composite stiffened panels. DLR Report IB 131-99/20, 1999.
-
(1999)
DLR Report
, vol.IB 131-99-20
-
-
Chai, Y.1
Gädke, M.2
-
15
-
-
0030102196
-
Computational models for sandwich panels and shells
-
Noor AK, Burton WS, Bert CW. Computational models for sandwich panels and shells. Appl Mech Rev 1996;49(3):155-99.
-
(1996)
Appl Mech Rev
, vol.49
, Issue.3
, pp. 155-199
-
-
Noor, A.K.1
Burton, W.S.2
Bert, C.W.3
-
17
-
-
0023347585
-
A generalization of two-dimensional theories of laminated composite plates
-
Reddy JN. A generalization of two-dimensional theories of laminated composite plates. Commun Appl Numer Methods 1987;3:173-80.
-
(1987)
Commun Appl Numer Methods
, vol.3
, pp. 173-180
-
-
Reddy, J.N.1
-
18
-
-
85015584826
-
Theories and computational models for composite laminates
-
Reddy JN, Robbins Jr. DH. Theories and computational models for composite laminates. Appl Mech Rev 1994;47(6):147-69.
-
(1994)
Appl Mech Rev
, vol.47
, Issue.6
, pp. 147-169
-
-
Reddy, J.N.1
Robbins Jr., D.H.2
-
19
-
-
0033249220
-
0 zig-zag kinematic displacement models for the analysis of laminated composites
-
0 zig-zag kinematic displacement models for the analysis of laminated composites. Mech Compos Mater Struct 1999;6(1):31-56.
-
(1999)
Mech Compos Mater Struct
, vol.6
, Issue.1
, pp. 31-56
-
-
Aitharaju, V.R.1
Averill, R.C.2
-
20
-
-
0033101698
-
0 zig-zag finite element for analysis of laminated composite beams
-
0 zig-zag finite element for analysis of laminated composite beams. J Eng Mech 1999;125(3):323-30.
-
(1999)
J Eng Mech
, vol.125
, Issue.3
, pp. 323-330
-
-
Aitharaju, V.R.1
Averill, R.C.2
-
21
-
-
0011211137
-
Numerical assessment of the core deformability effect on the behavior of sandwich beams
-
Di Sciuva M, Icardi U. Numerical assessment of the core deformability effect on the behavior of sandwich beams. Compos Struct 2001;52:41-53.
-
(2001)
Compos Struct
, vol.52
, pp. 41-53
-
-
Di Sciuva, M.1
Icardi, U.2
-
22
-
-
0035026534
-
Higher-order zig-zag model for analysis of thick composite beams with inclusion of transverse normal stress and sublaminates approximations
-
Icardi U. Higher-order zig-zag model for analysis of thick composite beams with inclusion of transverse normal stress and sublaminates approximations. Composites: Part B 2001;32:343-54.
-
(2001)
Composites: Part B
, vol.32
, pp. 343-354
-
-
Icardi, U.1
-
23
-
-
0037276698
-
Applications of zig-zag theories to sandwich beams
-
Icardi U. Applications of zig-zag theories to sandwich beams. Mech Adv Mater Struct 2003; 10(1):77-97.
-
(2003)
Mech Adv Mater Struct
, vol.10
, Issue.1
, pp. 77-97
-
-
Icardi, U.1
-
24
-
-
0028714043
-
A general sublaminate analysis method for determining strain energy release rates in composites
-
Flanagan G. A general sublaminate analysis method for determining strain energy release rates in composites. AIAA-94-1356 CP 1994. p. 381-9.
-
(1994)
AIAA-94-1356 CP
, pp. 381-389
-
-
Flanagan, G.1
-
25
-
-
0006417868
-
{1, 2}-Order theory for elastodynamic analysis of thick orthotropic shells
-
Tessler A, Tsui T, Saether E. A {1, 2}-order theory for elastodynamic analysis of thick orthotropic shells. Int J Solids Struct 1995;32(22):3237-60.
-
(1995)
Int J Solids Struct
, vol.32
, Issue.22
, pp. 3237-3260
-
-
Tessler, A.1
Tsui, T.2
Saether, E.A.3
-
26
-
-
0027097687
-
Multilayered anisotropic plate models with continuous mterlaminar stresses
-
Di Sciuva M. Multilayered anisotropic plate models with continuous mterlaminar stresses. Compos Struct 1992;22(3):149-68.
-
(1992)
Compos Struct
, vol.22
, Issue.3
, pp. 149-168
-
-
Di Sciuva, M.1
-
27
-
-
0024937168
-
Refinement of higher-order laminated plate theories
-
Bhaskar K, Varadan TK. Refinement of higher-order laminated plate theories. AIAA J 1989;27:1830-1.
-
(1989)
AIAA J
, vol.27
, pp. 1830-1831
-
-
Bhaskar, K.1
Varadan, T.K.2
-
28
-
-
85003297592
-
Interlaminar stress continuity theory for laminated composite analysis
-
Lee CY, Liu D. Interlaminar stress continuity theory for laminated composite analysis. AIAA J 1991;29:2010-2.
-
(1991)
AIAA J
, vol.29
, pp. 2010-2012
-
-
Lee, C.Y.1
Liu, D.2
-
29
-
-
38249005749
-
Nonlinear analysis of composite plates using interlaminar shear stress continuity theory
-
Lee CY, Liu D. Nonlinear analysis of composite plates using interlaminar shear stress continuity theory. Compos Eng 1993;3:151-68.
-
(1993)
Compos Eng
, vol.3
, pp. 151-168
-
-
Lee, C.Y.1
Liu, D.2
-
30
-
-
0027626987
-
Efficient higher order composite plate theory for general lamination configurations
-
Cho M, Parmerter R. Efficient higher order composite plate theory for general lamination configurations. AIAA J 1993;31(7):1299-306.
-
(1993)
AIAA J
, vol.31
, Issue.7
, pp. 1299-1306
-
-
Cho, M.1
Parmerter, R.2
-
31
-
-
3242850165
-
An efficient thick beam theory and finite element model with zig-zag sublaminates approximations
-
Averill RC, Yip YC. An efficient thick beam theory and finite element model with zig-zag sublaminates approximations. AIAA J 1996;34(8):1626-32.
-
(1996)
AIAA J
, vol.34
, Issue.8
, pp. 1626-1632
-
-
Averill, R.C.1
Yip, Y.C.2
-
32
-
-
0031628251
-
Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up
-
Icardi U. Eight-noded zig-zag element for deflection and stress analysis of plates with general lay-up. Composites: Part B 1998;29:435-41.
-
(1998)
Composites: Part B
, vol.29
, pp. 435-441
-
-
Icardi, U.1
-
33
-
-
0030733416
-
Improved transverse shear stress in composite finite elements based on first order shear deformation theory
-
Rolfes R, Rohwer K. Improved transverse shear stress in composite finite elements based on first order shear deformation theory. Int J Numer Methods Eng 1997;40:51-60.
-
(1997)
Int J Numer Methods Eng
, vol.40
, pp. 51-60
-
-
Rolfes, R.1
Rohwer, K.2
-
34
-
-
0032166331
-
Efficient linear transverse normal stress analysis of layered composite plates
-
Rolfes R. Efficient linear transverse normal stress analysis of layered composite plates. Comput Struct 1998;68:643-52.
-
(1998)
Comput Struct
, vol.68
, pp. 643-652
-
-
Rolfes, R.1
-
35
-
-
19744382320
-
Calculating three dimensional stresses in layered composite plates and shells
-
Rolfes R, Rohwer K. Calculating three dimensional stresses in layered composite plates and shells. Mech Composite Mater 1998;34(4):491-500.
-
(1998)
Mech Composite Mater
, vol.34
, Issue.4
-
-
Rolfes, R.1
Rohwer, K.2
-
36
-
-
9944224484
-
-
Degree dissertation, Turin Polytechnic, Faculty of Engineering, Department of Aeronautical and Spatial Engineering, Lecturer Prof. U. Icardi
-
Zardo G. Numerical and experimental investigation of composite, stiffened panels undertaking impact loading. Degree dissertation, Turin Polytechnic, Faculty of Engineering, Department of Aeronautical and Spatial Engineering, Lecturer Prof. U. Icardi, 2000.
-
(2000)
Numerical and Experimental Investigation of Composite, Stiffened Panels Undertaking Impact Loading
-
-
Zardo, G.1
-
37
-
-
38149144512
-
The displacement-type finite element approach - From art to science
-
Prathap G. The displacement-type finite element approach - from art to science. Prog Aerospace Sci 1994;10: 295-405.
-
(1994)
Prog Aerospace Sci
, vol.10
, pp. 295-405
-
-
Prathap, G.1
-
38
-
-
0030174799
-
Optimal strain location of two-dimensional continuum elements in terms of fieldconsistency
-
Yong-Woo K, Oak-Key M. Optimal strain location of two-dimensional continuum elements in terms of fieldconsistency. Comput Struct 1996;59(6):1121-38.
-
(1996)
Comput Struct
, vol.59
, Issue.6
, pp. 1121-1138
-
-
Yong-Woo, K.1
Oak-Key, M.2
-
39
-
-
0024699641
-
More on optimal stress points reduced integration, element distortions and error estimation
-
Barlow J. More on optimal stress points reduced integration, element distortions and error estimation. Int J Numer Methods Eng 1989;28:1486-504.
-
(1989)
Int J Numer Methods Eng
, vol.28
, pp. 1486-1504
-
-
Barlow, J.1
-
40
-
-
0016872745
-
Optimal stress location in finite element models
-
Barlow J. Optimal stress location in finite element models. Int J Numer Methods Eng 1976;10:243-51.
-
(1976)
Int J Numer Methods Eng
, vol.10
, pp. 243-251
-
-
Barlow, J.1
-
42
-
-
0019024701
-
Failure criteria for unidirectional fiber composites
-
Hashin ZH. Failure criteria for unidirectional fiber composites. J Appl Mech 1980;47:329-34.
-
(1980)
J Appl Mech
, vol.47
, pp. 329-334
-
-
Hashin, Z.H.1
-
43
-
-
0025741967
-
Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part I-analysis
-
Chang FK, Lessard H. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part I-analysis. J Comput Math 1991;25(1):2-43.
-
(1991)
J Comput Math
, vol.25
, Issue.1
, pp. 2-43
-
-
Chang, F.K.1
Lessard, H.2
-
44
-
-
0033894182
-
Finite element analysis of low velocity impact on composite sandwich plates
-
Palazotto AN. Finite element analysis of low velocity impact on composite sandwich plates. Compos Struct 2000;49:209-27.
-
(2000)
Compos Struct
, vol.49
, pp. 209-227
-
-
Palazotto, A.N.1
-
46
-
-
84964144652
-
Exact solutions for composite laminates in cylindrical bending
-
Pagano NJ. Exact solutions for composite laminates in cylindrical bending. J. Compos Mater 1969;3:398-411.
-
(1969)
J. Compos Mater
, vol.3
, pp. 398-411
-
-
Pagano, N.J.1
-
47
-
-
23844465000
-
0 element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating
-
submitted
-
0 element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updating. Int J Mech Sci, submitted.
-
Int J Mech Sci
-
-
Icardi, U.1
|