-
1
-
-
0025813702
-
-
Reid LF. Airframe life extension through cold expansion techniques. In: International Conference on Aircraft damage assessment and repair, Melbourne; 1991. p. 109-14.
-
Reid LF. Airframe life extension through cold expansion techniques. In: International Conference on Aircraft damage assessment and repair, Melbourne; 1991. p. 109-14.
-
-
-
-
2
-
-
0026736851
-
Effect of residual stress on the fatigue performance of the structure of a ballised hole
-
Lai M.O., Nee A.Y.C., and Oh J.T. Effect of residual stress on the fatigue performance of the structure of a ballised hole. J Mater Process Technol 29 (1992) 301-309
-
(1992)
J Mater Process Technol
, vol.29
, pp. 301-309
-
-
Lai, M.O.1
Nee, A.Y.C.2
Oh, J.T.3
-
3
-
-
0001673801
-
Fatigue crack propagation in light alloy steel material and structures
-
Pergamon Press, New York
-
Schijive J. Fatigue crack propagation in light alloy steel material and structures. Advances in aeronautical sciences (1961), Pergamon Press, New York 387-408
-
(1961)
Advances in aeronautical sciences
, pp. 387-408
-
-
Schijive, J.1
-
4
-
-
0026867583
-
A review on crack closure for single overload
-
Kumar R. A review on crack closure for single overload. Eng Fract Mech 42 1 (1992) 151-158
-
(1992)
Eng Fract Mech
, vol.42
, Issue.1
, pp. 151-158
-
-
Kumar, R.1
-
5
-
-
0009717453
-
Effect of loading parameters on post-overload fatigue crack closure
-
Verma B.B., Pandey R.K., and Chinnadurai R. Effect of loading parameters on post-overload fatigue crack closure. J Test Evaluat 26 6 (1998) 602-608
-
(1998)
J Test Evaluat
, vol.26
, Issue.6
, pp. 602-608
-
-
Verma, B.B.1
Pandey, R.K.2
Chinnadurai, R.3
-
6
-
-
0021649358
-
On the influence of the initial ∼K level on the post-overload crack propagation behaviour
-
Ranganathan N., Petit J., and Fougnet J.D. On the influence of the initial ∼K level on the post-overload crack propagation behaviour. Adv Fract Res 3 (1984) 1767-1774
-
(1984)
Adv Fract Res
, vol.3
, pp. 1767-1774
-
-
Ranganathan, N.1
Petit, J.2
Fougnet, J.D.3
-
7
-
-
56249133068
-
-
Sadananda K, Vasudevan AK. Analysis of fatigue crack closure and threshold. In: Erdogan F, editor. Fracture mechanics, vol. 25, ASTM STP; 1993. p. 484-501.
-
Sadananda K, Vasudevan AK. Analysis of fatigue crack closure and threshold. In: Erdogan F, editor. Fracture mechanics, vol. 25, ASTM STP; 1993. p. 484-501.
-
-
-
-
8
-
-
0033227627
-
eff estimation procedures on 6060-T6 and 2024-T3 aluminum alloys
-
eff estimation procedures on 6060-T6 and 2024-T3 aluminum alloys. Int J Fatigue 21 (1999) S47-S57
-
(1999)
Int J Fatigue
, vol.21
-
-
Donald, K.1
Paris, P.C.2
-
9
-
-
0035452427
-
0.5driving force parameter for crack growth in aluminum alloys
-
0.5driving force parameter for crack growth in aluminum alloys. Int J Fatigue 23 8 (2001) 733-740
-
(2001)
Int J Fatigue
, vol.23
, Issue.8
, pp. 733-740
-
-
Kujawski, D.1
-
10
-
-
0035214679
-
A fatigue crack driving force parameter with load ratio effects
-
Kujawski D. A fatigue crack driving force parameter with load ratio effects. Int J Fatigue 23 (2001) S239-S246
-
(2001)
Int J Fatigue
, vol.23
-
-
Kujawski, D.1
-
11
-
-
0027962720
-
A review of crack closure, fatigue crack threshold and related phenomena
-
Vasudevan A.K., Sadananda K., and Louat N. A review of crack closure, fatigue crack threshold and related phenomena. Mater Sci Eng A 188 1-2 (1994) 1-22
-
(1994)
Mater Sci Eng A
, vol.188
, Issue.1-2
, pp. 1-22
-
-
Vasudevan, A.K.1
Sadananda, K.2
Louat, N.3
-
13
-
-
27144502676
-
A two parameter driving force for fatigue crack growth analysis
-
Noroozi A.H., Glinka G., and Lambert S. A two parameter driving force for fatigue crack growth analysis. Int J Fatigue 27 (2005) 1277-1296
-
(2005)
Int J Fatigue
, vol.27
, pp. 1277-1296
-
-
Noroozi, A.H.1
Glinka, G.2
Lambert, S.3
-
14
-
-
56249090460
-
-
Willenborg JD, Engle RM, Wood HA. A crack growth retardation model using an effective stress concept. AFFDL, TM-71-1- FBR. OH: Air Force Flight Dynamics Laboratory, Wright Patterson Airforce Base; 1971.
-
Willenborg JD, Engle RM, Wood HA. A crack growth retardation model using an effective stress concept. AFFDL, TM-71-1- FBR. OH: Air Force Flight Dynamics Laboratory, Wright Patterson Airforce Base; 1971.
-
-
-
-
15
-
-
56249093546
-
-
NASA. Fatigue crack growth computer program. "NASGRO", version 3.0 - reference manual; 2000.
-
NASA. Fatigue crack growth computer program. "NASGRO", version 3.0 - reference manual; 2000.
-
-
-
-
16
-
-
0015316080
-
Spectrum loading and crack growth
-
Wheeler O.E. Spectrum loading and crack growth. J Basic Eng Trans ASME, Ser D 94 1 (1972) 181-186
-
(1972)
J Basic Eng Trans ASME, Ser D
, vol.94
, Issue.1
, pp. 181-186
-
-
Wheeler, O.E.1
-
17
-
-
0015055746
-
The significance of fatigue crack closure in fatigue
-
Elber W. The significance of fatigue crack closure in fatigue. ASTM STP 486 (1972) 230-242
-
(1972)
ASTM STP
, vol.486
, pp. 230-242
-
-
Elber, W.1
-
18
-
-
56249089425
-
-
Aliaga D, Davy A, Schaff H. Mechanics of fatigue crack closure. In: Newman JC Jr., editor; 1987; p. 491-504.
-
Aliaga D, Davy A, Schaff H. Mechanics of fatigue crack closure. In: Newman JC Jr., editor; 1987; p. 491-504.
-
-
-
-
19
-
-
56249143538
-
-
Padmadinata UH. Investigation of crack-closure prediction models for fatigue in aluminium alloy sheet under flight-simulation loading. PhD-thesis, Delft; 1990.
-
Padmadinata UH. Investigation of crack-closure prediction models for fatigue in aluminium alloy sheet under flight-simulation loading. PhD-thesis, Delft; 1990.
-
-
-
-
20
-
-
0006145973
-
-
Petit J., et al. (Ed), Elsevier Applied Science, London
-
Baudin G., Labourdette R., and Robert M. In: Petit J., et al. (Ed). Fatigue crack growth under variable amplitude loading (1988), Elsevier Applied Science, London 292-308
-
(1988)
Fatigue crack growth under variable amplitude loading
, pp. 292-308
-
-
Baudin, G.1
Labourdette, R.2
Robert, M.3
-
21
-
-
0019686176
-
A Simple crack closure model for prediction of fatigue crack growth rates under variable-amplitude loading
-
de Koning A.U. A Simple crack closure model for prediction of fatigue crack growth rates under variable-amplitude loading. ASTM STP 743 (1981) 63-85
-
(1981)
ASTM STP
, vol.743
, pp. 63-85
-
-
de Koning, A.U.1
-
22
-
-
0019627111
-
A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading
-
Newman Jr. J.C. A crack-closure model for predicting fatigue crack growth under aircraft spectrum loading. ASTM STP 748 (1981) 53-84
-
(1981)
ASTM STP
, vol.748
, pp. 53-84
-
-
Newman Jr., J.C.1
-
23
-
-
56249104516
-
-
de Koning AU, van der Linden HH. Prediction of fatigue crack growth rates under variable loading using a simple crack closure model. NLR MP 81023U, Amsterdam; 1981.
-
de Koning AU, van der Linden HH. Prediction of fatigue crack growth rates under variable loading using a simple crack closure model. NLR MP 81023U, Amsterdam; 1981.
-
-
-
-
24
-
-
0025207412
-
Effect of compressive and tensile overloads on fatigue damage accumulation in 2024-T351 aluminum
-
Pompetzki M.A., Topper T.H., Duquesnay D.L., and Yu M.T. Effect of compressive and tensile overloads on fatigue damage accumulation in 2024-T351 aluminum. J Test Evaluat 18 1 (1990) 53-61
-
(1990)
J Test Evaluat
, vol.18
, Issue.1
, pp. 53-61
-
-
Pompetzki, M.A.1
Topper, T.H.2
Duquesnay, D.L.3
Yu, M.T.4
-
25
-
-
0030111786
-
Analytical model of fatigue crack growth retardation due to overloading
-
Bolotin V.V., and Lebedev V.L. Analytical model of fatigue crack growth retardation due to overloading. Int J Solids Struct 33 9 (1996) 1229-1242
-
(1996)
Int J Solids Struct
, vol.33
, Issue.9
, pp. 1229-1242
-
-
Bolotin, V.V.1
Lebedev, V.L.2
-
26
-
-
0037911585
-
Fatigue analysis under variable amplitude loading using an energy parameter
-
Lee B.L., Kim K.S., and Nam K.M. Fatigue analysis under variable amplitude loading using an energy parameter. Int J Fatigue 25 (2003) 621-631
-
(2003)
Int J Fatigue
, vol.25
, pp. 621-631
-
-
Lee, B.L.1
Kim, K.S.2
Nam, K.M.3
-
28
-
-
33947385836
-
State-of-the-art review on fatigue crack growth analysis under variable amplitude loading
-
Murthy A.R.C., Palani G.S., and Iyer N.R. State-of-the-art review on fatigue crack growth analysis under variable amplitude loading. IE (I) J-CV 85 (2004) 118-129
-
(2004)
IE (I) J-CV
, vol.85
, pp. 118-129
-
-
Murthy, A.R.C.1
Palani, G.S.2
Iyer, N.R.3
-
30
-
-
56249100138
-
-
Brown WF, Srawley JE. Plane strain crack toughness testing of high strength metallic materials. ASTM STP, ASTM, Philadelphia, USA, vol. 410. 1966. p. 1.
-
Brown WF, Srawley JE. Plane strain crack toughness testing of high strength metallic materials. ASTM STP, ASTM, Philadelphia, USA, vol. 410. 1966. p. 1.
-
-
-
-
31
-
-
56249097319
-
-
Irwin GR. NRL Report 6598; November 21, 1967.
-
Irwin GR. NRL Report 6598; November 21, 1967.
-
-
-
-
32
-
-
21244499415
-
A study on spot heating induced fatigue crack growth retardation
-
Ray P.K., Ray P.K., and Verma B.B. A study on spot heating induced fatigue crack growth retardation. Fat Fract Eng Mat Struct 28 (2005) 579-585
-
(2005)
Fat Fract Eng Mat Struct
, vol.28
, pp. 579-585
-
-
Ray, P.K.1
Ray, P.K.2
Verma, B.B.3
|