-
1
-
-
34147111601
-
COCOMAT - Improved MATerial Exploitation at Safe Design of Composite Airframe Structures by Accurate Simulation of COllapse
-
R. Degenhardt, R. Rolfes, R. Zimmerman and K. Rohwer, "COCOMAT - Improved MATerial Exploitation at Safe Design of Composite Airframe Structures by Accurate Simulation of COllapse," Comp. Struct., 73, 178-178 (2006).
-
(2006)
Comp. Struct
, vol.73
, pp. 178-178
-
-
Degenhardt, R.1
Rolfes, R.2
Zimmerman, R.3
Rohwer, K.4
-
2
-
-
34147180871
-
-
COCOMAT Home Page, www.cocomat.de (2006).
-
COCOMAT Home Page, www.cocomat.de (2006).
-
-
-
-
4
-
-
0031622801
-
Interlaminar fracture toughness: The long and winding road to standardization
-
T. K. O'Brien, "Interlaminar fracture toughness: The long and winding road to standardization," Composites, B, 29, 57-62 (1998).
-
(1998)
Composites, B
, vol.29
, pp. 57-62
-
-
O'Brien, T.K.1
-
5
-
-
0017561766
-
A finite element calculation of stress intensity factors by a modified crack closure integral
-
E. F. Rybicki and M. F. Kanninen, "A finite element calculation of stress intensity factors by a modified crack closure integral," Eng. Fract. Mech., 9, 931-938 (1977).
-
(1977)
Eng. Fract. Mech
, vol.9
, pp. 931-938
-
-
Rybicki, E.F.1
Kanninen, M.F.2
-
6
-
-
0027148902
-
Computation of local energy release rates along straight and curved delamination fronts of unidirectionally laminated DCB- and ENF-specimens
-
La Jolla, CA, AIAA Washington
-
R. Krüger, M. König, and T. Schneider, "Computation of local energy release rates along straight and curved delamination fronts of unidirectionally laminated DCB- and ENF-specimens," in: Proc. of the 34th AIAA/ASME/ASCE/AHS/ASC SSDM Conf., La Jolla, CA, AIAA Washington (1993), pp. 1332-1342.
-
(1993)
Proc. of the 34th AIAA/ASME/ASCE/AHS/ASC SSDM Conf
, pp. 1332-1342
-
-
Krüger, R.1
König, M.2
Schneider, T.3
-
7
-
-
0031188311
-
Evaluation of the edge crack torsion ECT Test for mode III interlaminar fracture toughness of laminated composites
-
J. Li, S. M. Lee, E. W. Lee, and T. K. O'Brien, "Evaluation of the edge crack torsion ECT Test for mode III interlaminar fracture toughness of laminated composites," J. Comp. Technol. Res., 19, 174-183 (1997).
-
(1997)
J. Comp. Technol. Res
, vol.19
, pp. 174-183
-
-
Li, J.1
Lee, S.M.2
Lee, E.W.3
O'Brien, T.K.4
-
8
-
-
0000673848
-
On the use of fracture mechanics in designing a single lap adhesive joint
-
M. M. A. Wahab, "On the use of fracture mechanics in designing a single lap adhesive joint," J. Adhes. Sci. Technol., 19, 851-865 (2000).
-
(2000)
J. Adhes. Sci. Technol
, vol.19
, pp. 851-865
-
-
Wahab, M.M.A.1
-
9
-
-
19944378921
-
Nonlinear numerical and experimental analysis of single lap adhesive composite joints with delaminated adherends
-
Y. Zhang ed, Beijing
-
M. Qin and Y. Dzenis, "Nonlinear numerical and experimental analysis of single lap adhesive composite joints with delaminated adherends," in: Y. Zhang (ed.), Proc. of the 13th Int. Conf. on Composite Materials (ICCM13), Beijing (2001).
-
(2001)
Proc. of the 13th Int. Conf. on Composite Materials (ICCM13)
-
-
Qin, M.1
Dzenis, Y.2
-
10
-
-
0030151023
-
Strain energy release rate formulae for skin-stiffener debond modeled with plate elements
-
J. T. Wang and I. S. Raju, "Strain energy release rate formulae for skin-stiffener debond modeled with plate elements," Eng. Fract. Mech., 54, 211-228 (1996).
-
(1996)
Eng. Fract. Mech
, vol.54
, pp. 211-228
-
-
Wang, J.T.1
Raju, I.S.2
-
11
-
-
0009828716
-
-
J. Li, T. K. O'Brien, and C. Q. Rousseau, Test and analysis of composite hat stringer pull-off test specimens, J. Amer. Heli. Soc., 350-357 (1997).
-
J. Li, T. K. O'Brien, and C. Q. Rousseau, "Test and analysis of composite hat stringer pull-off test specimens," J. Amer. Heli. Soc., 350-357 (1997).
-
-
-
-
12
-
-
34147183102
-
-
W. S. Johnson, L. M. Butkus, and R. V. Valentin, Applications of Fracture Mechanics to the Durability of Bonded Composite Joints, U.S. Department of Transportation, Federal Aviation Administration DOT/FAA/AR-97/56 (1998).
-
W. S. Johnson, L. M. Butkus, and R. V. Valentin, Applications of Fracture Mechanics to the Durability of Bonded Composite Joints, U.S. Department of Transportation, Federal Aviation Administration DOT/FAA/AR-97/56 (1998).
-
-
-
-
13
-
-
0013400840
-
-
NASA/CR-2002-211628, ICASE Virginia, USA
-
R. Krueger, The Virtual Crack Closure Technique: History, Approach, and Applications, NASA/CR-2002-211628, ICASE Virginia, USA (2002).
-
(2002)
The Virtual Crack Closure Technique: History, Approach, and Applications
-
-
Krueger, R.1
-
14
-
-
3242690863
-
-
NASA/TM-2002-211737, NASA Langley Research Center, Virginia, USA
-
P. P. Camanho and C. G. Davila, Mixed-Mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials, NASA/TM-2002-211737, NASA Langley Research Center, Virginia, USA (2002).
-
(2002)
Mixed-Mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials
-
-
Camanho, P.P.1
Davila, C.G.2
-
15
-
-
0031619186
-
Progressive delamination using interface elements
-
Y. Mi, M. A. Crisfield and G. A. O. Davies, "Progressive delamination using interface elements," J. Compos. Mater., 32, No. 14, 1246-1272 (1998).
-
(1998)
J. Compos. Mater
, vol.32
, Issue.14
, pp. 1246-1272
-
-
Mi, Y.1
Crisfield, M.A.2
Davies, G.A.O.3
-
16
-
-
34147128488
-
Development of a degradation model for the collapse analysis of composite aerospace structures
-
C. A. Mota Soares et al, eds, Lisbon, Portugal, 5-9 June
-
A. C. Orifici, R. S. Thomson, R. Degenhardt, C. Bisagni, and J. Bayandor, "Development of a degradation model for the collapse analysis of composite aerospace structures," in: C. A. Mota Soares et al. (eds), Proc. of the 3rd Europ. Conf. on Computational Mechanics: Solids, Structures and Coupled Problems in Engineering, Lisbon, Portugal, 5-9 June (2006).
-
(2006)
Proc. of the 3rd Europ. Conf. on Computational Mechanics: Solids, Structures and Coupled Problems in Engineering
-
-
Orifici, A.C.1
Thomson, R.S.2
Degenhardt, R.3
Bisagni, C.4
Bayandor, J.5
-
17
-
-
4143145183
-
Influence of post-buckling behaviour of composite stiffened panels on the damage criticality
-
J. W. H. Yap, R. S. Thomson, M. L. Scott, and D. Hachenberg, "Influence of post-buckling behaviour of composite stiffened panels on the damage criticality," Comp. Struct., 66, 197-206 (2004).
-
(2004)
Comp. Struct
, vol.66
, pp. 197-206
-
-
Yap, J.W.H.1
Thomson, R.S.2
Scott, M.L.3
Hachenberg, D.4
-
18
-
-
34147125206
-
-
Version 2005, MSC.Software Corporation, Santa Ana, CA
-
MSC.Marc and MSC.Mentat User Manuals Version 2005, MSC.Software Corporation, Santa Ana, CA (2004).
-
(2004)
User Manuals
-
-
Marc, M.S.C.1
Mentat, M.S.C.2
-
19
-
-
34147160508
-
-
ed, Handbook der Physik1958, pp
-
G. R. Irwin, "Fracture I," in: Flügge (ed.), Handbook der Physik(1958), pp. 558-590.
-
Fracture I
, pp. 558-590
-
-
Irwin, G.R.1
-
20
-
-
84970692230
-
An analytical investigation of delamination front curvature in double cantilever beam specimens
-
B. D. Davidson, "An analytical investigation of delamination front curvature in double cantilever beam specimens," J. Compos. Mater., 24, 1124-1137 (1990).
-
(1990)
J. Compos. Mater
, vol.24
, pp. 1124-1137
-
-
Davidson, B.D.1
-
21
-
-
0342803672
-
Experimental aspects of Mode I and Mode II fracture toughness testing of fibre-reinforced polymer-matrix composites
-
A. J. Brunner, "Experimental aspects of Mode I and Mode II fracture toughness testing of fibre-reinforced polymer-matrix composites," Comput. Meth. Appl. Mech. Eng., 185, 161-172 (2000).
-
(2000)
Comput. Meth. Appl. Mech. Eng
, vol.185
, pp. 161-172
-
-
Brunner, A.J.1
-
22
-
-
34147121323
-
Characterization of Material Properties
-
Results of the EU Project COCOMAT, IB 131-2006/18 April
-
A. Kling and R. Degenhardt, Characterization of Material Properties, Results of the EU Project COCOMAT, Internal DLR Report, IB 131-2006/18 (April, 2006).
-
(2006)
Internal DLR Report
-
-
Kling, A.1
Degenhardt, R.2
-
23
-
-
84864179186
-
-
IC. European Normative Standard DIN EN 6033, Deutsches Institut für Normung, e. V. (1996).
-
IC. European Normative Standard DIN EN 6033, Deutsches Institut für Normung, e. V. (1996).
-
-
-
|