-
1
-
-
76049118094
-
-
Modular joints for aircraft components (MOJO). Research project funded by the European commission within the frame of 6th framework - aeronautics and space. Description of Work; 2006.
-
Modular joints for aircraft components (MOJO). Research project funded by the European commission within the frame of 6th framework - aeronautics and space. Description of Work; 2006.
-
-
-
-
2
-
-
0032206524
-
Three-dimensional stress analysis of bolted single-composite joints
-
Ireman T. Three-dimensional stress analysis of bolted single-composite joints. Compos Struct 43 (1998) 195-216
-
(1998)
Compos Struct
, vol.43
, pp. 195-216
-
-
Ireman, T.1
-
3
-
-
0036794556
-
Strength prediction of bolted joints in graphite/epoxy composite laminates
-
Tserpes K.I., Labeas G., Papanikos P., and Kermanidis Th. Strength prediction of bolted joints in graphite/epoxy composite laminates. Composites Part B 33 (2002) 521-529
-
(2002)
Composites Part B
, vol.33
, pp. 521-529
-
-
Tserpes, K.I.1
Labeas, G.2
Papanikos, P.3
Kermanidis, Th.4
-
4
-
-
0034299816
-
Adhesive bonding of aircraft structures
-
Higgins A. Adhesive bonding of aircraft structures. Int J Adhes Adhes 20 (2000) 367-376
-
(2000)
Int J Adhes Adhes
, vol.20
, pp. 367-376
-
-
Higgins, A.1
-
5
-
-
0019896944
-
A review of the strength of joints in fibre-reinforced plastics
-
Matthews F.L., Kilty P.F., and Godwin E.W. A review of the strength of joints in fibre-reinforced plastics. Composites (1982) 29-37
-
(1982)
Composites
, pp. 29-37
-
-
Matthews, F.L.1
Kilty, P.F.2
Godwin, E.W.3
-
6
-
-
0348039966
-
Finite element prediction of fatigue crack propagation lifetime in composite bonded joints
-
Abdel Wahab M.M., Ashcroft I.A., Crocombe A.D., and Smith P.A. Finite element prediction of fatigue crack propagation lifetime in composite bonded joints. Composites Part A 35 (2004) 213-222
-
(2004)
Composites Part A
, vol.35
, pp. 213-222
-
-
Abdel Wahab, M.M.1
Ashcroft, I.A.2
Crocombe, A.D.3
Smith, P.A.4
-
7
-
-
0029715770
-
Analysis of concrete beams reinforced with externally bonded woven composite fabrics
-
Kaliakin V.N., Chajes M.J., and Januszka T.F. Analysis of concrete beams reinforced with externally bonded woven composite fabrics. Composites Part B 27B (1996) 235-244
-
(1996)
Composites Part B
, vol.27 B
, pp. 235-244
-
-
Kaliakin, V.N.1
Chajes, M.J.2
Januszka, T.F.3
-
8
-
-
0034784532
-
Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends I. Experimental
-
Potter K.D., Guild F.J., Harvey H.J., Wisnom M.R., and Adams R.D. Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends I. Experimental. Int J Adhes Adhes 21 (2001) 435-443
-
(2001)
Int J Adhes Adhes
, vol.21
, pp. 435-443
-
-
Potter, K.D.1
Guild, F.J.2
Harvey, H.J.3
Wisnom, M.R.4
Adams, R.D.5
-
9
-
-
0034784491
-
Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends II. Finite element analysis
-
Guild F.J., Potter K.D., Heinrich J., Adams R.D., and Wisnom M.R. Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends II. Finite element analysis. Int J Adhes Adhes 21 (2001) 445-453
-
(2001)
Int J Adhes Adhes
, vol.21
, pp. 445-453
-
-
Guild, F.J.1
Potter, K.D.2
Heinrich, J.3
Adams, R.D.4
Wisnom, M.R.5
-
10
-
-
34447289825
-
Dimensionless parameters in symmetric double lap joints: an orthotropic solution for thermomechanical loading
-
Gustafson P.A., Bizard A., and Waas A.M. Dimensionless parameters in symmetric double lap joints: an orthotropic solution for thermomechanical loading. Int J Solids Struct 44 (2007) 5774-5795
-
(2007)
Int J Solids Struct
, vol.44
, pp. 5774-5795
-
-
Gustafson, P.A.1
Bizard, A.2
Waas, A.M.3
-
11
-
-
68649116545
-
A bonded joint finite element for a symmetric double lap joint subjected to mechanical and thermal loads
-
Gustafson P.A., and Waas A.M. A bonded joint finite element for a symmetric double lap joint subjected to mechanical and thermal loads. Int J Numer Methods Eng 79 (2009) 94-126
-
(2009)
Int J Numer Methods Eng
, vol.79
, pp. 94-126
-
-
Gustafson, P.A.1
Waas, A.M.2
-
12
-
-
70349507789
-
Prediction of delamination in braided composite T-piece specimens
-
Chen J., Ravey E., Hallett S., Wisnom M., and Grassi M. Prediction of delamination in braided composite T-piece specimens. Compos Sci Technol 69 (2009) 2363-2367
-
(2009)
Compos Sci Technol
, vol.69
, pp. 2363-2367
-
-
Chen, J.1
Ravey, E.2
Hallett, S.3
Wisnom, M.4
Grassi, M.5
-
13
-
-
62649090593
-
The influence of adhesive constitutive parameters in cohesive zone finite element models of adhesively bonded joints
-
Gustafson P.A., and Waas A.M. The influence of adhesive constitutive parameters in cohesive zone finite element models of adhesively bonded joints. Int J Solids Struct 46 (2009) 2201-2215
-
(2009)
Int J Solids Struct
, vol.46
, pp. 2201-2215
-
-
Gustafson, P.A.1
Waas, A.M.2
-
14
-
-
52749099864
-
Mesomechanical analysis of composite non-crimp fabric structural parts
-
Tserpes K.I., and Labeas G. Mesomechanical analysis of composite non-crimp fabric structural parts. Compos Struct 87 (2009) 358-369
-
(2009)
Compos Struct
, vol.87
, pp. 358-369
-
-
Tserpes, K.I.1
Labeas, G.2
-
15
-
-
0033116527
-
Observations in the structural response of adhesive bondline defects
-
Heslehurst R.B. Observations in the structural response of adhesive bondline defects. Int J Adhes Adhes 19 (1999) 133-154
-
(1999)
Int J Adhes Adhes
, vol.19
, pp. 133-154
-
-
Heslehurst, R.B.1
-
16
-
-
76049116850
-
-
2-liquid epoxy resin 180 °C curing - material specification.
-
2-liquid epoxy resin 180 °C curing - material specification.
-
-
-
-
17
-
-
76049109077
-
-
AIMS 05-04-011: airbus material specification - HR carbon biaxial noncrimp fabric 0/90 with epoxy resin 180 °C curing - material specification.
-
AIMS 05-04-011: airbus material specification - HR carbon biaxial noncrimp fabric 0/90 with epoxy resin 180 °C curing - material specification.
-
-
-
-
18
-
-
76049096392
-
-
AIMS 05-04-007: airbus material specification - HR carbon biaxial noncrimp fabric +45/-45//-45/+45 with epoxy resin, 180 °C curing/Liba tech - material specification.
-
AIMS 05-04-007: airbus material specification - HR carbon biaxial noncrimp fabric +45/-45//-45/+45 with epoxy resin, 180 °C curing/Liba tech - material specification.
-
-
-
-
20
-
-
33745741576
-
Squeeze flow characterization of thermoplastic polymer
-
Jackson A.P., Liu X.-L., and Paton R. Squeeze flow characterization of thermoplastic polymer. Compos Struct 75 (2006) 179-184
-
(2006)
Compos Struct
, vol.75
, pp. 179-184
-
-
Jackson, A.P.1
Liu, X.-L.2
Paton, R.3
-
21
-
-
76049106714
-
-
AITM 1.0019: airbus industries test method - determination of tensile lap shear strength of composite joints.
-
AITM 1.0019: airbus industries test method - determination of tensile lap shear strength of composite joints.
-
-
-
-
22
-
-
76049117337
-
-
ANSYS 11.0 documentation; 2007.
-
ANSYS 11.0 documentation; 2007.
-
-
-
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