-
1
-
-
0141877261
-
Glare: History of the development of a new aircraft material
-
Kluwer Academic Publishers
-
A. Vlot Glare: History of the development of a new aircraft material 2002 Kluwer Academic Publishers
-
(2002)
-
-
Vlot, A.1
-
2
-
-
0003679362
-
Towards Glare - The development of a fatigue insensitive and damage tolerant aircraft material
-
Ph.D. Thesis Delft University of Technology, Delft
-
Roebroeks G. Towards Glare - the development of a fatigue insensitive and damage tolerant aircraft material, Ph.D. Thesis, Delft University of Technology, Delft, 1991.
-
(1991)
-
-
Roebroeks, G.1
-
3
-
-
31144463589
-
Flying Glare® - A contribution to aircraft certification issues on strengths properties in non-damaged and fatigue damaged Glare® structures
-
Ph.D. Thesis, Delft University of Technology, Delft
-
Beumler Th. Flying Glare® - A contribution to aircraft certification issues on strengths properties in non-damaged and fatigue damaged Glare® structures Ph.D. Thesis, Delft University of Technology, Delft, 2004
-
(2004)
-
-
Beumler, T.H.1
-
4
-
-
31144442131
-
An empirical crack growth model for fiber/metal laminates
-
Melbourne, Australia 18th Symposium of the International Committee on Aeronautical Fatigue
-
Toi R. An empirical crack growth model for fiber/metal laminates. In: 18th Symposium of the International Committee on Aeronautical Fatigue, Melbourne, Australia, 1995.
-
(1995)
-
-
Toi, R.1
-
6
-
-
0041738988
-
Evaluation of fatigue crack growth behaviour of Glare3 fiber/metal laminates using compliance method
-
T. Takamatsu T. Shimokawa T. Matsumura Y. Miyoshi Y. Tanabe Evaluation of fatigue crack growth behaviour of Glare3 fiber/metal laminates using compliance method Engng Fract Mech 70 2003 2603-2616
-
(2003)
Engng Fract Mech
, vol.70
, pp. 2603-2616
-
-
Takamatsu, T.1
Shimokawa, T.2
Matsumura, T.3
Miyoshi, Y.4
Tanabe, Y.5
-
7
-
-
0032754743
-
A phenomenological model for predicting crack growth in fiber-reinforced metal laminates under constant-amplitude loading
-
Y.J. Guo X.R. Wu A phenomenological model for predicting crack growth in fiber-reinforced metal laminates under constant-amplitude loading Comput Sci Technol 59 1999 1825-1831
-
(1999)
Comput Sci Technol
, vol.59
, pp. 1825-1831
-
-
Guo, Y.J.1
Wu, X.R.2
-
8
-
-
0003598657
-
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, Delft
-
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, Delft, 1988.
-
(1988)
-
-
Marissen, R.1
-
9
-
-
0032678227
-
Bridging stress distribution in a center-cracked fiber reinforced metal laminates: Modelling and experiment
-
X.J. Guo X.R. Wu Bridging stress distribution in a center-cracked fiber reinforced metal laminates: Modelling and experiment Engng Fract Mech 63 1999 147-163
-
(1999)
Engng Fract Mech
, vol.63
, pp. 147-163
-
-
Guo, X.J.1
Wu, X.R.2
-
10
-
-
0029219452
-
Effect of fiber bridging on the fatigue crack propagation in carbon fiber-reinforced aluminium laminates
-
C.T. Lin P.W. Kao Effect of fiber bridging on the fatigue crack propagation in carbon fiber-reinforced aluminium laminates Mater Sci Engng A 190 1995 65-73
-
(1995)
Mater Sci Engng A
, vol.190
, pp. 65-73
-
-
Lin, C.T.1
Kao, P.W.2
-
11
-
-
1942455903
-
Crack tunneling and plane-strain delamination in layered solids
-
A.S.J. Suiker N.A. Fleck Crack tunneling and plane-strain delamination in layered solids Int J Fract 125 2004 1-32
-
(2004)
Int J Fract
, vol.125
, pp. 1-32
-
-
Suiker, A.S.J.1
Fleck, N.A.2
|