-
1
-
-
67349149016
-
Tango metallic fuselage barrel validation of advanced technologies
-
Rouchon J, editor, ICAF, Cepadues Editionss
-
Schmidt HJ, Voto C, Hansson J. Tango metallic fuselage barrel validation of advanced technologies. In: Rouchon J, editor. Proceedings of the 21st symposium of the international committee on aeronautical fatigue, ICAF, Cepadues Editionss; 2001. p. 273-88.
-
(2001)
Proceedings of the 21st symposium of the international committee on aeronautical fatigue
, pp. 273-88
-
-
Schmidt, H.J.1
Voto, C.2
Hansson, J.3
-
4
-
-
0025658501
-
Crack stoppers and arall laminates
-
Schijve J. Crack stoppers and arall laminates. Engng Fract Mech 1990, 37(2):405-421.
-
(1990)
Engng Fract Mech
, vol.37
, Issue.2
, pp. 405-421
-
-
Schijve, J.1
-
5
-
-
34547509948
-
Improving damage tolerance of aircraft structures through the use of selective reinforcement
-
Proceedings 23rd symposium of international committee on aeronautical fatigue (ICAF), Hamburg
-
Heinimann MB, Bucci RJ, Kulak M, Garratt M. Improving damage tolerance of aircraft structures through the use of selective reinforcement. In: Proceedings 23rd symposium of international committee on aeronautical fatigue (ICAF), Hamburg; 2005. p. 197-208.
-
(2005)
, pp. 197-208
-
-
Heinimann, M.B.1
Bucci, R.J.2
Kulak, M.3
Garratt, M.4
-
6
-
-
22544435815
-
Damage tolerance and fail safety of welded aircraft wing panels
-
Zhang X., Li Y. Damage tolerance and fail safety of welded aircraft wing panels. AIAA J 2005, 43(7):1613-1623.
-
(2005)
AIAA J
, vol.43
, Issue.7
, pp. 1613-1623
-
-
Zhang, X.1
Li, Y.2
-
7
-
-
34748899948
-
Adhesively bonded cfrp straps as fatigue crack growth retarders on aa2024-t3
-
Long Beach
-
Colavita M, Bowler A. Zhang X. Irving PE. Adhesively bonded cfrp straps as fatigue crack growth retarders on aa2024-t3. In: SAMPE 2006, Long Beach; 2006.
-
(2006)
-
-
Colavita, M.1
Bowler, A.2
Zhang, X.3
Irving P.E4
-
9
-
-
51749094192
-
Design and modelling of selective reinforcements for integral aircraft structures
-
Boscolo M., Allegri G., Zhang X. Design and modelling of selective reinforcements for integral aircraft structures. AIAA J 2008, 46(9):2323-2331.
-
(2008)
AIAA J
, vol.46
, Issue.9
, pp. 2323-2331
-
-
Boscolo, M.1
Allegri, G.2
Zhang, X.3
-
10
-
-
79952605059
-
Improving fail-safety of aircraft integral structures through the use of bonded crack retarders
-
Naples;
-
Zhang X, Figueroa-Gordon D, Boscolo M, Allegri G, Irving PE. Improving fail-safety of aircraft integral structures through the use of bonded crack retarders. in: Proceedings 24th symposium of international committee on aeronautical fatigue (ICAF), Naples; 2007.
-
(2007)
Proceedings 24th symposium of international committee on aeronautical fatigue (ICAF)
-
-
Zhang, X.1
Figueroa-Gordon, D.2
Boscolo, M.3
Allegri, G.4
Irving, P.E.5
-
11
-
-
57649229234
-
Fail-safe design of integral metallic aircraft structures reinforced by bonded crack retarders
-
Zhang X., Boscolo M., Figueroa-Gordon D., Allegri G., Irving P.E. Fail-safe design of integral metallic aircraft structures reinforced by bonded crack retarders. Engng Fract Mech 2009, 76:114-133.
-
(2009)
Engng Fract Mech
, vol.76
, pp. 114-133
-
-
Zhang, X.1
Boscolo, M.2
Figueroa-Gordon, D.3
Allegri, G.4
Irving, P.E.5
-
12
-
-
77949914904
-
A modelling technique for calculating stress intensity factors for structures reinforced by bonded straps. Part II: validation
-
Boscolo M., Zhang X. A modelling technique for calculating stress intensity factors for structures reinforced by bonded straps. Part II: validation. Engng Fract Mech 2010, 77(6):896-907.
-
(2010)
Engng Fract Mech
, vol.77
, Issue.6
, pp. 896-907
-
-
Boscolo, M.1
Zhang, X.2
-
13
-
-
34547512156
-
Software tools for analysis of bonded joints
-
542. NASA/GSFC;
-
Tahmasebi F. Software tools for analysis of bonded joints. Tech. rep. 542. NASA/GSFC; 2001.
-
(2001)
Tech. rep.
-
-
Tahmasebi, F.1
-
14
-
-
84973010670
-
Influence of rotatory inertia and shear on flexural vibrations of isotropic, elastic plates
-
Mindlin R.D. Influence of rotatory inertia and shear on flexural vibrations of isotropic, elastic plates. J Appl Mech 1951, 18:1031-1036.
-
(1951)
J Appl Mech
, vol.18
, pp. 1031-1036
-
-
Mindlin, R.D.1
-
15
-
-
0017561766
-
A finite element calculation of stress intensity factors by a modified crack closure integral
-
Rybicki E., Kanninen M. A finite element calculation of stress intensity factors by a modified crack closure integral. Engng Fract Mech 1977, 9:931-938.
-
(1977)
Engng Fract Mech
, vol.9
, pp. 931-938
-
-
Rybicki, E.1
Kanninen, M.2
-
16
-
-
0023599309
-
Calculation of strain energy release rate with higher order and singular finite elements
-
Raju I. Calculation of strain energy release rate with higher order and singular finite elements. Engng Fract Mech 1987, 28:251-274.
-
(1987)
Engng Fract Mech
, vol.28
, pp. 251-274
-
-
Raju, I.1
-
17
-
-
0013400840
-
The virtual crack closure technique: history, approach and applications
-
Report No. 2002-10 NASA/CR-2002-211628, ICASE, ICASE Mail Stop 132C NASA Langley Research Center Hampton;
-
Krueger R. The virtual crack closure technique: history, approach and applications. Report No. 2002-10 NASA/CR-2002-211628, ICASE, ICASE Mail Stop 132C NASA Langley Research Center Hampton; 2002.
-
(2002)
-
-
Krueger, R.1
-
18
-
-
0004038972
-
Standard test method for plane-strain fracture toughness of metallic materials
-
E399-90. Annual book of ASTM standards
-
Standard test method for plane-strain fracture toughness of metallic materials. E399-90. Annual book of ASTM standards; 1993.
-
(1993)
-
-
-
20
-
-
0032058107
-
Analysis of out-of-plane bending in one-sided bonded repair
-
Wang C.H., Rose L.R.F., Callinan R. Analysis of out-of-plane bending in one-sided bonded repair. Int J Solids Struct 1998, 35(14):1653-1675.
-
(1998)
Int J Solids Struct
, vol.35
, Issue.14
, pp. 1653-1675
-
-
Wang, C.H.1
Rose, L.R.F.2
Callinan, R.3
-
21
-
-
0033133803
-
A crack bridging model for bonded plates subjected to tension and bending
-
Wang C.H., Rose L.R.F. A crack bridging model for bonded plates subjected to tension and bending. Int J Solids Struct 1999, 36:1985-2014.
-
(1999)
Int J Solids Struct
, vol.36
, pp. 1985-2014
-
-
Wang, C.H.1
Rose, L.R.F.2
-
22
-
-
0027573267
-
On the strain energy release rate for cracked plate subjected to out-of-plane bending moment
-
Young M., Sun C.T. On the strain energy release rate for cracked plate subjected to out-of-plane bending moment. Int J Fract 1993, 60:227-247.
-
(1993)
Int J Fract
, vol.60
, pp. 227-247
-
-
Young, M.1
Sun, C.T.2
-
24
-
-
0030079820
-
Analysis of cracked aluminium plates repaired with bonded composite patches
-
Sun C.T., Klung J., Arendt C. Analysis of cracked aluminium plates repaired with bonded composite patches. AIAA J 1996, 34(2):369-374.
-
(1996)
AIAA J
, vol.34
, Issue.2
, pp. 369-374
-
-
Sun, C.T.1
Klung, J.2
Arendt, C.3
-
25
-
-
0033336375
-
Characterization of fatigue behavior of bonded composite repairs
-
Klug J., Maley S., Sun C.T. Characterization of fatigue behavior of bonded composite repairs. J Aircraft 1999, 36(6):1016-1022.
-
(1999)
J Aircraft
, vol.36
, Issue.6
, pp. 1016-1022
-
-
Klug, J.1
Maley, S.2
Sun, C.T.3
-
26
-
-
67650895672
-
Enhanced 2D modelling technique for single-sided patch patches
-
Boscolo M., Allegri G., Zhang X. Enhanced 2D modelling technique for single-sided patch patches. AIAA J 2009, 47(6):1558-1567.
-
(2009)
AIAA J
, vol.47
, Issue.6
, pp. 1558-1567
-
-
Boscolo, M.1
Allegri, G.2
Zhang, X.3
-
27
-
-
24144465687
-
Fatigue behavior of composite patch repaired aluminum plate
-
Lee W.-Y., Lee J.-J. Fatigue behavior of composite patch repaired aluminum plate. J Compos Mater 2005, 39(16):1449-1463.
-
(2005)
J Compos Mater
, vol.39
, Issue.16
, pp. 1449-1463
-
-
Lee, W.-Y.1
Lee, J.-J.2
-
28
-
-
4143101255
-
Successive 3d fe analysis technique for characterization of fatigue crack growth behavior in composite-repaired aluminum plate
-
Lee W.-Y., Lee J.-J. Successive 3d fe analysis technique for characterization of fatigue crack growth behavior in composite-repaired aluminum plate. Compos Struct 2004, 66:513-520.
-
(2004)
Compos Struct
, vol.66
, pp. 513-520
-
-
Lee, W.-Y.1
Lee, J.-J.2
-
29
-
-
85158842538
-
Characterising growth in graphite-epoxy
-
[aSTM STP 775]
-
Wilkins DJ, Eisenmann J, Camin R, Margolis W, Benson R. Characterising growth in graphite-epoxy. In: Damage in composite materials; 1982. p. 168-83 [aSTM STP 775].
-
(1982)
Damage in composite materials;
, pp. 168-183
-
-
Wilkins, D.J.1
Eisenmann, J.2
Camin, R.3
Margolis, W.4
Benson, R.5
-
31
-
-
31144475111
-
Application of the energy release rate approach for delamination growth in glare
-
Alderliesten R., Schijve J., van der Zwaag S. Application of the energy release rate approach for delamination growth in glare. Engng Fract Mech 2006, 73:697-709.
-
(2006)
Engng Fract Mech
, vol.73
, pp. 697-709
-
-
Alderliesten, R.1
Schijve, J.2
van der Zwaag, S.3
-
32
-
-
1542505609
-
Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates
-
Andersons J., Hojo M., Ochiai S. Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates. Int J Fatigue 2004, 26:597-604.
-
(2004)
Int J Fatigue
, vol.26
, pp. 597-604
-
-
Andersons, J.1
Hojo, M.2
Ochiai, S.3
-
34
-
-
0029327903
-
Growth of internal delamination under cyclic compression in composite plates
-
Kardomateas G., Pelegri A., Malik B. Growth of internal delamination under cyclic compression in composite plates. J Mech Phys Solids 1995, 43(6):847-868.
-
(1995)
J Mech Phys Solids
, vol.43
, Issue.6
, pp. 847-868
-
-
Kardomateas, G.1
Pelegri, A.2
Malik, B.3
-
35
-
-
27444438189
-
A total fatigue life model for mode i delaminated composite laminates
-
Shivakumara K., Chena H., Abalib F., Leb D., Davis C. A total fatigue life model for mode i delaminated composite laminates. Int J Fatigue 1995, 28:33-42.
-
(1995)
Int J Fatigue
, vol.28
, pp. 33-42
-
-
Shivakumara, K.1
Chena, H.2
Abalib, F.3
Leb, D.4
Davis, C.5
-
36
-
-
0036294264
-
Determination of mode II fatigue delamination toughness of laminated composites
-
Vinciquerra A.J., Davinson B., Schaff J., Smith S.L. Determination of mode II fatigue delamination toughness of laminated composites. J Reinf Plast Compos 2002, 21(07):663-677.
-
(2002)
J Reinf Plast Compos
, vol.21
, Issue.7
, pp. 663-677
-
-
Vinciquerra, A.J.1
Davinson, B.2
Schaff, J.3
Smith, S.L.4
-
37
-
-
31144468495
-
Strain energy release rate calculation for moving delamination front of arbitrary shape based on the virtual crack closure technique. Part I: formulation and validation
-
Xie D., Biggers S. Strain energy release rate calculation for moving delamination front of arbitrary shape based on the virtual crack closure technique. Part I: formulation and validation. Engng Fract Mech 2006, 73:771-785.
-
(2006)
Engng Fract Mech
, vol.73
, pp. 771-785
-
-
Xie, D.1
Biggers, S.2
-
38
-
-
31144475373
-
Strain energy release rate calculation for moving delamination front of arbitrary shape based on the virtual crack closure technique. Part II: sensitivity study on modeling details
-
Xie D., Biggers S. Strain energy release rate calculation for moving delamination front of arbitrary shape based on the virtual crack closure technique. Part II: sensitivity study on modeling details. Engng Fract Mech 2006, 73:786-801.
-
(2006)
Engng Fract Mech
, vol.73
, pp. 786-801
-
-
Xie, D.1
Biggers, S.2
-
39
-
-
3242690863
-
Mixed-mode decohesion finite elements for the simulation of delamination in composite materials
-
TM-2002-211737. NASA; June 2002.
-
Camanho PP, Dàvila C. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. Tech. rep. TM-2002-211737. NASA; June 2002.
-
Tech. rep.
-
-
Camanho, P.P.1
Dàvila, C.2
-
40
-
-
0026714175
-
Modeling compression failure of laminated composites contain multiple through-the-width delaminations
-
Kutlu Z., Chang F. Modeling compression failure of laminated composites contain multiple through-the-width delaminations. Compos Mater 1992, 26(3):350-387.
-
(1992)
Compos Mater
, vol.26
, Issue.3
, pp. 350-387
-
-
Kutlu, Z.1
Chang, F.2
-
43
-
-
0034353726
-
Geometrically linear analysis of thermal stresses in one-sided composite repairs
-
Wang C.H., Erjavec D. Geometrically linear analysis of thermal stresses in one-sided composite repairs. J Therm Stress 2000, 23:833-851.
-
(2000)
J Therm Stress
, vol.23
, pp. 833-851
-
-
Wang, C.H.1
Erjavec, D.2
-
44
-
-
0032024955
-
Composite patches as reinforcements and crack arrestors in aircraft structures
-
Lena M.R., Klug J., Sun C.T. Composite patches as reinforcements and crack arrestors in aircraft structures. J Aircraft 1998, 35(2):318-324.
-
(1998)
J Aircraft
, vol.35
, Issue.2
, pp. 318-324
-
-
Lena, M.R.1
Klug, J.2
Sun, C.T.3
-
45
-
-
0018737372
-
Effect of residual stresses on fatigue crack growth in steel weldments under constant and variable amplitude load
-
STP 677. ASTM;
-
Glinka G. Effect of residual stresses on fatigue crack growth in steel weldments under constant and variable amplitude load. Tech. Rep. STP 677. ASTM; 1979.
-
(1979)
Tech. Rep.
-
-
Glinka, G.1
-
46
-
-
0000698668
-
Effects of residual stress on fatigue crack propagation
-
STP 776. ASTM;
-
Nelson DV. Effects of residual stress on fatigue crack propagation. Tech. Rep. STP 776. ASTM; 1982.
-
(1982)
Tech. Rep.
-
-
Nelson, D.V.1
-
47
-
-
67349221039
-
Predicting fatigue crack growth rate in a welded butt joint: the role of effective R ratio in accounting for residual stress effect
-
Servetti G., Zhang X. Predicting fatigue crack growth rate in a welded butt joint: the role of effective R ratio in accounting for residual stress effect. Engng Fract Mech 2009, 76(11):1589-1602.
-
(2009)
Engng Fract Mech
, vol.76
, Issue.11
, pp. 1589-1602
-
-
Servetti, G.1
Zhang, X.2
-
48
-
-
12344257819
-
-
Duong C.N., Wang C.H., repair On the characterization of fatigue crack growth in a plate with a single-sided J Engng Mater Technol 2004, 126:192-198.
-
(2004)
J Engng Mater Technol
, vol.126
, pp. 192-198
-
-
Duong, C.N.1
Wang, C.H.2
-
49
-
-
33847634229
-
A simple method to calculate the crack growth life of adhesively repaired aluminum panels
-
Hosseini-Toudeshky H., Mohammadi B. A simple method to calculate the crack growth life of adhesively repaired aluminum panels. Compos Struct 2007, 79:234-241.
-
(2007)
Compos Struct
, vol.79
, pp. 234-241
-
-
Hosseini-Toudeshky, H.1
Mohammadi, B.2
-
50
-
-
0003823170
-
-
Air vehicles directorate, afrl-va-wp-tr-2006-xxxx edition; June 2006
-
Harter J. AFGROW users guide and technical manual. Air vehicles directorate, afrl-va-wp-tr-2006-xxxx edition; June 2006.
-
AFGROW users guide and technical manual
-
-
Harter, J.1
|