-
2
-
-
0040729578
-
Bonded repair of damage
-
[2] Jones R. Bonded repair of damage. J Aero Soc (India) 1984;36:193-201.
-
(1984)
J Aero Soc (India)
, vol.36
, pp. 193-201
-
-
Jones, R.1
-
3
-
-
0019392130
-
An application of the inclusion analogy for bonded reinforcements
-
[3] Rose LRF. An application of the inclusion analogy for bonded reinforcements. Int J Solids Structures 1981;17:827-838.
-
(1981)
Int J Solids Structures
, vol.17
, pp. 827-838
-
-
Rose, L.R.F.1
-
4
-
-
0002531767
-
Bending effects on unsymmetric dahesively bonded composite repairs on cracked aluminum panels
-
Hampton, VA, 4-6 May
-
[4] Sun CT, Arendt C. Bending effects on unsymmetric dahesively bonded composite repairs on cracked aluminum panels. In: Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance (Hampton, VA, 4-6 May 1994), vol. I, pp. 33-48.
-
(1994)
Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
, vol.1
, pp. 33-48
-
-
Sun, C.T.1
Arendt, C.2
-
5
-
-
0030079820
-
Analysis of cracked aluminum plates repaired with bonded composite patches
-
[5] Sun CT, Klug J, Arendt C. Analysis of cracked aluminum 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
Klug, J.2
Arendt, C.3
-
6
-
-
0027097448
-
Analysis of patched and stiffened cracked panels using the boundary element method
-
[6] Young MJ, Rooke DP, Cartwright DJ. Analysis of patched and stiffened cracked panels using the boundary element method. Int J Solids Structures 1992;29:(17):2201-2216.
-
(1992)
Int J Solids Structures
, vol.29
, Issue.17
, pp. 2201-2216
-
-
Young, M.J.1
Rooke, D.P.2
Cartwright, D.J.3
-
7
-
-
0017913959
-
A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures
-
[7] Ratwani MM. A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures. J Eng Mater Technol 1978;100:46-51.
-
(1978)
J Eng Mater Technol
, vol.100
, pp. 46-51
-
-
Ratwani, M.M.1
-
8
-
-
0018517116
-
Analysis of cracked adhesively bonded laminated structures
-
[8] Ratwani MM. Analysis of cracked adhesively bonded laminated structures. AIAA J 1979;17:988-994.
-
(1979)
AIAA J
, vol.17
, pp. 988-994
-
-
Ratwani, M.M.1
-
9
-
-
0013314907
-
Characterization of fatigue crack growth in bonded structures - Analysis of cracked bonded structures
-
Air Force Flight Dynamics Laboratory, OH, July
-
[9] Ratwani MM. Characterization of fatigue crack growth in bonded structures - analysis of cracked bonded structures. AFFADL-TR-31, vol. II. Air Force Flight Dynamics Laboratory, OH, July 1977.
-
(1977)
AFFADL-TR-31
, vol.2
-
-
Ratwani, M.M.1
-
10
-
-
0013314907
-
Characterization of fatigue crack growth in bonded structures - Crack growth prediction in bonded structures
-
Air Force Flight Dynamics Laboratory, OH, July
-
[10] Ratwani MM. Characterization of fatigue crack growth in bonded structures - crack growth prediction in bonded structures. AFFADL-TR-31, vol. I. Air Force Flight Dynamics Laboratory, OH, July 1977.
-
(1977)
AFFADL-TR-31
, vol.1
-
-
Ratwani, M.M.1
-
11
-
-
0030197458
-
Modeling of cracked metallic structure with bonded composite patch using three layer technique
-
[11] Naboulsi S, Mall S. Modeling of cracked metallic structure with bonded composite patch using three layer technique. Composite Structures 1996;35:295-308.
-
(1996)
Composite Structures
, vol.35
, pp. 295-308
-
-
Naboulsi, S.1
Mall, S.2
-
12
-
-
0030834515
-
Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels
-
[12] Naboulsi S, Mall S. Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels. Theor. Appl. Fract. Mech. 1996;26:1-12.
-
(1996)
Theor. Appl. Fract. Mech.
, vol.26
, pp. 1-12
-
-
Naboulsi, S.1
Mall, S.2
-
13
-
-
0031084182
-
Characterization of fatigue crack growth in aluminum panels with bonded composite patch
-
[13] Naboulsi S, Mall S. Characterization of fatigue crack growth in aluminum panels with bonded composite patch. Composite Structures 1997;37:321-334.
-
(1997)
Composite Structures
, vol.37
, pp. 321-334
-
-
Naboulsi, S.1
Mall, S.2
-
14
-
-
0031247090
-
Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches
-
[14] Naboulsi S, Mall S. Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches. Theor Appl Fract Mech 1997;28:13-28.
-
(1997)
Theor Appl Fract Mech
, vol.28
, pp. 13-28
-
-
Naboulsi, S.1
Mall, S.2
-
15
-
-
0017561766
-
A finite element calculation of stress intensity factors by a modified crack closure integral
-
[15] Rybicki EF, Kanninen EF. A finite element calculation of stress intensity factors by a modified crack closure integral. Eng Fract Mech 1977;9:931-938.
-
(1977)
Eng Fract Mech
, vol.9
, pp. 931-938
-
-
Rybicki, E.F.1
Kanninen, E.F.2
-
16
-
-
0032108260
-
Large deflection effects of cracked aluminum plates repaired with bonded composite patches
-
in press
-
[16] Klug J, Sun CT. Large deflection effects of cracked aluminum plates repaired with bonded composite patches. Composite Structures, in press.
-
Composite Structures
-
-
Klug, J.1
Sun, C.T.2
-
17
-
-
0040729577
-
-
Hibbitt, Karlsson and Sorensen, Inc. Pawtucket, RI 02860, USA
-
[17] ABAQUS Finite Element Programs, ABAQUS/Standard 5.6. Hibbitt, Karlsson and Sorensen, Inc. Pawtucket, RI 02860, USA, 1994.
-
(1994)
ABAQUS Finite Element Programs, ABAQUS/standard 5.6
-
-
-
18
-
-
0040729580
-
-
personal communication. Wright Laboratory, OH
-
[18] Mazza J, personal communication. Wright Laboratory, OH.
-
-
-
Mazza, J.1
-
19
-
-
0040729576
-
Crack growth in imperfectly bonded composite patch repairs of cracked aluminium panels
-
ICAF 97, Fatigue in New and Ageing Aircraft, 18-20 June Edinburgh, UK.
-
[19] Naboulsi S, Mall S, Denney JJ. Crack growth in imperfectly bonded composite patch repairs of cracked aluminium panels. In ICAF 97, Fatigue in New and Ageing Aircraft, Proceedings of the 19th Symposium of the International Committee on Aeronautical Fatigue, 18-20 June 1997, Edinburgh, UK. Vol. 1, pp. 639-655.
-
(1997)
Proceedings of the 19th Symposium of the International Committee on Aeronautical Fatigue
, vol.1
, pp. 639-655
-
-
Naboulsi, S.1
Mall, S.2
Denney, J.J.3
-
21
-
-
0029722795
-
Effect of disbond on fatigue behavior of cracked aluminum panel with bonded composite patch
-
Salt Lake City, UT, 15-17 April
-
[21] Denney JJ, Mall S. Effect of disbond on fatigue behavior of cracked aluminum panel with bonded composite patch. In Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Strcutural Dynamics, and Material Conferenc (Salt Lake City, UT, 15-17 April 1996), vol. I, pp. 14-21.
-
(1996)
Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Strcutural Dynamics, and Material Conferenc
, vol.1
, pp. 14-21
-
-
Denney, J.J.1
Mall, S.2
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