-
2
-
-
56949107537
-
-
Vlot A. Towards technology readiness of Fibre Metal Laminates - GLARE Technology Development 1997-2000. in: Proceedings of the 22nd International Congress of Aeronautical Sciences, Harrogate, United Kingdom, 2000. p. 1-15
-
Vlot A. Towards technology readiness of Fibre Metal Laminates - GLARE Technology Development 1997-2000. in: Proceedings of the 22nd International Congress of Aeronautical Sciences, Harrogate, United Kingdom, 2000. p. 1-15
-
-
-
-
3
-
-
56949088900
-
-
Vermeeren CAJR. The application of carbon fibres in ARALL laminates. Report LR-658, Delft University of Technology, 1991.
-
Vermeeren CAJR. The application of carbon fibres in ARALL laminates. Report LR-658, Delft University of Technology, 1991.
-
-
-
-
4
-
-
56949107814
-
-
Kleinendorst RGJ. Corrosion properties of carbon ARALL. Master Thesis, Delft University of Technology, 1990.
-
Kleinendorst RGJ. Corrosion properties of carbon ARALL. Master Thesis, Delft University of Technology, 1990.
-
-
-
-
5
-
-
0026124253
-
Fatigue behaviour of carbon fibre-reinforced aluminium laminates
-
Lin C.T., Kao P.W., and Yang F.S. Fatigue behaviour of carbon fibre-reinforced aluminium laminates. Composites 22 2 (1991) 135-141
-
(1991)
Composites
, vol.22
, Issue.2
, pp. 135-141
-
-
Lin, C.T.1
Kao, P.W.2
Yang, F.S.3
-
6
-
-
0030105682
-
Delamination growth and its effect on crack propagation in carbon fiber reinforced aluminum laminates under fatigue loading
-
Lin C.T., and Kao P.W. Delamination growth and its effect on crack propagation in carbon fiber reinforced aluminum laminates under fatigue loading. Acta Mater 44 3 (1996) 1181-1188
-
(1996)
Acta Mater
, vol.44
, Issue.3
, pp. 1181-1188
-
-
Lin, C.T.1
Kao, P.W.2
-
7
-
-
0030259069
-
Residual strength of centrally cracked metal/fiber composite laminates
-
Jin Z.-H., and Batra R.C. Residual strength of centrally cracked metal/fiber composite laminates. Mater Sci Eng A216 (1996) 117-124
-
(1996)
Mater Sci Eng
, vol.A216
, pp. 117-124
-
-
Jin, Z.-H.1
Batra, R.C.2
-
8
-
-
0035252024
-
Delamination growth from face sheet seams in cross-ply titanium/graphite hybrid laminates
-
Burianek D.A., and Spearing S.M. Delamination growth from face sheet seams in cross-ply titanium/graphite hybrid laminates. Compos Sci Technol 61 2 (2001) 261-269
-
(2001)
Compos Sci Technol
, vol.61
, Issue.2
, pp. 261-269
-
-
Burianek, D.A.1
Spearing, S.M.2
-
9
-
-
0036535004
-
Fatigue damage in titanium-graphite hybrid laminates
-
Burianek D.A., and Spearing S.M. Fatigue damage in titanium-graphite hybrid laminates. Compos Sci Technol 62 5 (2002) 607-617
-
(2002)
Compos Sci Technol
, vol.62
, Issue.5
, pp. 607-617
-
-
Burianek, D.A.1
Spearing, S.M.2
-
10
-
-
1042277650
-
Fracture properties of a fiber-metal laminates based on magnesium alloy
-
Cortés P., and Cantwell W.J. Fracture properties of a fiber-metal laminates based on magnesium alloy. J Mater Sci 39 (2004) 1081-1083
-
(2004)
J Mater Sci
, vol.39
, pp. 1081-1083
-
-
Cortés, P.1
Cantwell, W.J.2
-
11
-
-
28644439540
-
The fracture properties of a fibre-metal laminate based on magnesium alloy
-
Cortés P., and Cantwell W.J. The fracture properties of a fibre-metal laminate based on magnesium alloy. Composites B 37 (2006) 163-170
-
(2006)
Composites B
, vol.37
, pp. 163-170
-
-
Cortés, P.1
Cantwell, W.J.2
-
12
-
-
56949108442
-
-
AeroMag. Aeronautical application of wrought magnesium. A proposal for the 6th European framework program, FP6-2003-Aero-1, 2006.
-
AeroMag. Aeronautical application of wrought magnesium. A proposal for the 6th European framework program, FP6-2003-Aero-1, 2006.
-
-
-
-
13
-
-
34248574564
-
Evaluation of the anti-corrosive effect of acid pickling and sol-gel coating on magnesium AZ31 alloy
-
Supplit R., Koch Th., and Schubert U. Evaluation of the anti-corrosive effect of acid pickling and sol-gel coating on magnesium AZ31 alloy. Corros Sci 49 (2007) 3015-3023
-
(2007)
Corros Sci
, vol.49
, pp. 3015-3023
-
-
Supplit, R.1
Koch, Th.2
Schubert, U.3
-
14
-
-
56949089151
-
-
Roebroeks G. The Metal Volume Fraction approach. Report TD-R-00-003, Structural Laminates Industry, Delft, 2000.
-
Roebroeks G. The Metal Volume Fraction approach. Report TD-R-00-003, Structural Laminates Industry, Delft, 2000.
-
-
-
-
15
-
-
30344438821
-
Fatigue initiation in Fibre Metal Laminates
-
Homan J.J. Fatigue initiation in Fibre Metal Laminates. Int J Fatigue 28 (2006) 366-374
-
(2006)
Int J Fatigue
, vol.28
, pp. 366-374
-
-
Homan, J.J.1
-
16
-
-
33745950625
-
Fatigue and damage tolerance issues of Glare in aircraft structures
-
Alderlieste R.C. Fatigue and damage tolerance issues of Glare in aircraft structures. Int J Fatigue 28 (2006) 1116-1123
-
(2006)
Int J Fatigue
, vol.28
, pp. 1116-1123
-
-
Alderlieste, R.C.1
-
17
-
-
56949101393
-
-
Marissen R. Fatigue crack growth in ARALL, A hybrid Aluminium-Aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. Ph.D. Thesis, Delft University of Technology, 1988.
-
Marissen R. Fatigue crack growth in ARALL, A hybrid Aluminium-Aramid composite material, crack growth mechanisms and quantitative predictions of the crack growth rate. Ph.D. Thesis, Delft University of Technology, 1988.
-
-
-
-
18
-
-
56949091747
-
-
® structures. Ph.D. Dissertation, Delft University of Technology, 2004.
-
® structures. Ph.D. Dissertation, Delft University of Technology, 2004.
-
-
-
-
19
-
-
33845625682
-
Analytical prediction model for fatigue crack propagation and delamination growth in Glare
-
Alderliesten R.C. Analytical prediction model for fatigue crack propagation and delamination growth in Glare. Int J Fatigue 29 (2007) 628-646
-
(2007)
Int J Fatigue
, vol.29
, pp. 628-646
-
-
Alderliesten, R.C.1
-
20
-
-
56949093090
-
Shear yield strength
-
Kluwer Academic Publishers, Dordrecht, The Netherlands
-
Hagenbeek M. Shear yield strength. Fibre Metal Laminates, an introduction (2001), Kluwer Academic Publishers, Dordrecht, The Netherlands
-
(2001)
Fibre Metal Laminates, an introduction
-
-
Hagenbeek, M.1
-
21
-
-
56949105745
-
Blunt notch strength
-
Kluwer Academic Publishers, Dordrecht, The Netherlands
-
Bosker O.J. Blunt notch strength. Fibre Metal Laminates, an introduction (2001), Kluwer Academic Publishers, Dordrecht, The Netherlands
-
(2001)
Fibre Metal Laminates, an introduction
-
-
Bosker, O.J.1
-
22
-
-
56949099916
-
-
de Vries TJ. Blunt and sharp notch behaviour of Glare laminates. Ph.D. Thesis, Delft University of Technology, 2001.
-
de Vries TJ. Blunt and sharp notch behaviour of Glare laminates. Ph.D. Thesis, Delft University of Technology, 2001.
-
-
-
-
23
-
-
56949092170
-
-
ASM International. Fatigue data book: light structural alloys. ASM International, Materials Park, OH, USA, 1995.
-
ASM International. Fatigue data book: light structural alloys. ASM International, Materials Park, OH, USA, 1995.
-
-
-
-
24
-
-
56949083139
-
-
www.matweb.com.
-
www.matweb.com.
-
-
-
-
25
-
-
56949102952
-
-
MIL-HDBK 5H. Metallic materials and elements for aerospace vehicle structures. Department of Defence, USA, 1998.
-
MIL-HDBK 5H. Metallic materials and elements for aerospace vehicle structures. Department of Defence, USA, 1998.
-
-
-
-
26
-
-
56949087122
-
-
Alderliesten RC. Fatigue crack propagation and delamination growth in Glare. Ph.D. Thesis, Delft University of Technology, 2005.
-
Alderliesten RC. Fatigue crack propagation and delamination growth in Glare. Ph.D. Thesis, Delft University of Technology, 2005.
-
-
-
-
28
-
-
0032754743
-
A phenomenological model for predicting crack growth in fiber-reinforced metal laminates under constant-amplitude loading
-
Guo Y.J., and Wu X.R. A phenomenological model for predicting crack growth in fiber-reinforced metal laminates under constant-amplitude loading. Compos Sci Technol 59 12 (1999) 1825-1831
-
(1999)
Compos Sci Technol
, vol.59
, Issue.12
, pp. 1825-1831
-
-
Guo, Y.J.1
Wu, X.R.2
-
29
-
-
3242705130
-
Fatigue behaviour and fracture mechanism of a rolled AZ31 magnesium alloy
-
Tokaji K., Kamakura M., Ishiizumi Y., and Hasegawa N. Fatigue behaviour and fracture mechanism of a rolled AZ31 magnesium alloy. Int J Fatigue 26 (2004) 1217-1224
-
(2004)
Int J Fatigue
, vol.26
, pp. 1217-1224
-
-
Tokaji, K.1
Kamakura, M.2
Ishiizumi, Y.3
Hasegawa, N.4
-
30
-
-
56949097392
-
-
Schijve J. Some formulas for the crack opening stress level. Memorandum M-368, Delft University of Technology, Delft, 1980.
-
Schijve J. Some formulas for the crack opening stress level. Memorandum M-368, Delft University of Technology, Delft, 1980.
-
-
-
-
31
-
-
0028494999
-
Use of rule of mixtures and metal volume fraction for mechanical property predictions of fibre-reinforced aluminum laminates
-
Wu H.F., Wu L.L., Slagter W.J., and Verolme J.L. Use of rule of mixtures and metal volume fraction for mechanical property predictions of fibre-reinforced aluminum laminates. J Mater Sci 29 17 (1994) 4583-4591
-
(1994)
J Mater Sci
, vol.29
, Issue.17
, pp. 4583-4591
-
-
Wu, H.F.1
Wu, L.L.2
Slagter, W.J.3
Verolme, J.L.4
-
32
-
-
0041409502
-
The determination of the in-plane shear characteristics of aluminum alloys
-
Gilmour K.R., Leacock A.G., and Ashbridge M.T.J. The determination of the in-plane shear characteristics of aluminum alloys. J Test Eval 29 2 (2001) 131-137
-
(2001)
J Test Eval
, vol.29
, Issue.2
, pp. 131-137
-
-
Gilmour, K.R.1
Leacock, A.G.2
Ashbridge, M.T.J.3
-
33
-
-
31144475111
-
Application of the Energy Release Rate approach for delamination growth in Glare
-
April
-
Alderliesten R.C. Application of the Energy Release Rate approach for delamination growth in Glare. Eng Fract Mech 73 6 (2006) 697-709 April
-
(2006)
Eng Fract Mech
, vol.73
, Issue.6
, pp. 697-709
-
-
Alderliesten, R.C.1
-
34
-
-
56949108276
-
-
Alderliesten RC. Damage tolerance of bonded aircraft structures. In: Proceedings of the first international conference on damage tolerance of aircraft structures, September 25-28, Delft, The Netherlands, 2007.
-
Alderliesten RC. Damage tolerance of bonded aircraft structures. In: Proceedings of the first international conference on damage tolerance of aircraft structures, September 25-28, Delft, The Netherlands, 2007.
-
-
-
-
35
-
-
0017416714
-
Experimental confirmation of the J integral as thin section fracture criterion
-
Hickerson Jr. J.P. Experimental confirmation of the J integral as thin section fracture criterion. Eng Fract Mech 9 (1977) 75-85
-
(1977)
Eng Fract Mech
, vol.9
, pp. 75-85
-
-
Hickerson Jr., J.P.1
-
36
-
-
56949100184
-
-
Broek D. Effect of finite specimen width on residual strength of light alloy sheet, vol. V33. Reports and Trans. Amsterdam: National Aerospace Laboratory; 1968. p. 1-141.
-
Broek D. Effect of finite specimen width on residual strength of light alloy sheet, vol. V33. Reports and Trans. Amsterdam: National Aerospace Laboratory; 1968. p. 1-141.
-
-
-
-
37
-
-
56949104757
-
-
William D Callister Jr. Materials science and engineering: an introduction. 7th ed. ISBN 978-0-471-73696-7, 2007, 832 pp.
-
William D Callister Jr. Materials science and engineering: an introduction. 7th ed. ISBN 978-0-471-73696-7, 2007, 832 pp.
-
-
-
|