nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Analysis and prediction of microstructural effects on long-term fatigue performance of an aluminum aerospace alloy
|
Magnusen, P.E |
|
1997 |
19 |
93 |
p. 275-283 9 p. |
artikel |
2 |
Analysis of high temperature fatigue crack growth behavior
|
Sadananda, K |
|
1997 |
19 |
93 |
p. 183-189 7 p. |
artikel |
3 |
Analytical modeling for life extension of aging equipment
|
Sire, R.A |
|
1997 |
19 |
93 |
p. 261-266 6 p. |
artikel |
4 |
A new life extension method for high cycle fatigue using micro-martensitic transformation in an austenitic stainless steel 1 This work was carried out as a part of the Ph.D. thesis of one of the authors (T.H.M.). 1
|
Myeong, T.H. |
|
1997 |
19 |
93 |
p. 69-73 5 p. |
artikel |
5 |
Assessment of fatigue load spectrum from fracture surface topography
|
Kobayashi, Takao |
|
1997 |
19 |
93 |
p. 237-244 8 p. |
artikel |
6 |
Characterization of crack tip and geometry induced closure
|
Evans, W.J. |
|
1997 |
19 |
93 |
p. 205-210 6 p. |
artikel |
7 |
Cumulative fatigue damage modeling—crack nucleation and early growth
|
Halford, Gary R |
|
1997 |
19 |
93 |
p. 253-260 8 p. |
artikel |
8 |
Cyclic relaxation in compression-dominated structures
|
Tuegel, Eric J |
|
1997 |
19 |
93 |
p. 245-251 7 p. |
artikel |
9 |
Damage mechanisms of single and polycrystalline nickel base superalloys SC16 and IN738LC under high temperature LCF loading
|
Wahi, R.P. |
|
1997 |
19 |
93 |
p. 89-94 6 p. |
artikel |
10 |
Dwell sensitive fatigue in a near alpha titanium alloy at ambient temperature
|
Bache, M.R |
|
1997 |
19 |
93 |
p. 83-88 6 p. |
artikel |
11 |
Effective strain–fatigue life data for variable amplitude fatigue
|
Topper, T.H. |
|
1997 |
19 |
93 |
p. 137-143 7 p. |
artikel |
12 |
Effects of grain size on cyclic plasticity and fatigue crack initiation in nickel
|
Morrison, D.J. |
|
1997 |
19 |
93 |
p. 51-59 9 p. |
artikel |
13 |
Environmental interactions with fatigue crack growth in alpha/beta titanium alloys
|
Evans, W.J. |
|
1997 |
19 |
93 |
p. 177-182 6 p. |
artikel |
14 |
Fatigue analysis and the local stress–strain approach in complex vehicular structures
|
Conle, F.A. |
|
1997 |
19 |
93 |
p. 317-323 7 p. |
artikel |
15 |
Fatigue crack growth from stage I to stage II in a corrosive environment
|
Hamano, Ryuichi |
|
1997 |
19 |
93 |
p. 197-204 8 p. |
artikel |
16 |
Fatigue crack growth threshold: implications, determination and data evaluation
|
Döker, H. |
|
1997 |
19 |
93 |
p. 145-149 5 p. |
artikel |
17 |
Fatigue crack initiation and growth in riveted specimens: an optical and acoustic microscopic study
|
Connor, Z.M. |
|
1997 |
19 |
93 |
p. 331-337 7 p. |
artikel |
18 |
Fatigue crack initiation in alpha-beta titanium alloys
|
Hall, J.A |
|
1997 |
19 |
93 |
p. 23-37 15 p. |
artikel |
19 |
Fatigue crack initiation in Ti–5Al–4Sn–2Zr–1Mo–0.7Nd–0.25Si high temperature titanium alloy
|
Lei, J.F |
|
1997 |
19 |
93 |
p. 95-98 4 p. |
artikel |
20 |
Fatigue growth of small corner cracks in aluminum 6061-T651
|
Carlson, R.L |
|
1997 |
19 |
93 |
p. 119-125 7 p. |
artikel |
21 |
Fatigue issues in aircraft maintenance and repairs
|
Goranson, Ulf G. |
|
1997 |
19 |
93 |
p. 3-21 19 p. |
artikel |
22 |
Fatigue microcrack distributions and the reliability of a nickel base superalloy
|
Chen, E.Y. |
|
1997 |
19 |
93 |
p. 75-82 8 p. |
artikel |
23 |
Fatigue performance of 6261-T6 aluminium alloy – constant and variable amplitude loading of parent plate and welded specimens 1 This work was performed while M.N.J. was with the School of Process and Materials Engineering, University of the Witwatersrand, WITS 2050, South Africa. 1
|
James, M.N |
|
1997 |
19 |
93 |
p. 109-118 10 p. |
artikel |
24 |
Fretting fatigue in engineering alloys
|
Lindley, T.C. |
|
1997 |
19 |
93 |
p. 39-49 11 p. |
artikel |
25 |
Introducing the compliance ratio concept for determining effective stress intensity
|
Donald, J.Keith |
|
1997 |
19 |
93 |
p. 191-195 5 p. |
artikel |
26 |
Microstructural fracture in metal fatigue
|
Lawson, L. |
|
1997 |
19 |
93 |
p. 61-67 7 p. |
artikel |
27 |
Microstructure based fatigue life predictions for thick plate 7050-T7451 airframe alloys
|
Przystupa, Marek A |
|
1997 |
19 |
93 |
p. 285-288 4 p. |
artikel |
28 |
Modeling of cyclic stress–strain behavior and damage mechanisms under thermomechanical fatigue conditions
|
Maier, H.J |
|
1997 |
19 |
93 |
p. 267-274 8 p. |
artikel |
29 |
Multiaxial fatigue life prediction method in the ground vehicle industry
|
Chu, C.-C |
|
1997 |
19 |
93 |
p. 325-330 6 p. |
artikel |
30 |
Multiaxial small fatigue crack growth in metals
|
McDowell, David L. |
|
1997 |
19 |
93 |
p. 127-135 9 p. |
artikel |
31 |
Observation of fatigue damage in structural steel by scanning atomic force microscopy
|
Nakai, Yoshikazu |
|
1997 |
19 |
93 |
p. 223-236 14 p. |
artikel |
32 |
Physical meaning of ΔK RP and fatigue crack propagation in the residual stress distribution field
|
Toyosada, Masashiro |
|
1997 |
19 |
93 |
p. 161-166 6 p. |
artikel |
33 |
Prediction uncertainties at variable amplitude fatigue
|
Svensson, Thomas |
|
1997 |
19 |
93 |
p. 295-302 8 p. |
artikel |
34 |
Role of microstructures on the growth of long fatigue cracks
|
Vasudevan, A.K |
|
1997 |
19 |
93 |
p. 151-159 9 p. |
artikel |
35 |
Short crack growth and internal stresses
|
Sadananda, K |
|
1997 |
19 |
93 |
p. 99-108 10 p. |
artikel |
36 |
The effect of stress ratio on fatigue crack growth rate in the absence of closure
|
Sunder, R |
|
1997 |
19 |
93 |
p. 211-221 11 p. |
artikel |
37 |
The effects of load sequencing on the fatigue life of 2024-T3 aluminum alloy
|
Everett Jr., Richard A |
|
1997 |
19 |
93 |
p. 289-293 5 p. |
artikel |
38 |
The growth of cracks in Ti–6Al–4V plate under combined high and low cycle fatigue
|
Powell, B.E |
|
1997 |
19 |
93 |
p. 167-176 10 p. |
artikel |
39 |
Thickness effects on the fatigue strength of welded steel cruciforms
|
Kihl, David P |
|
1997 |
19 |
93 |
p. 311-316 6 p. |
artikel |
40 |
Unique fatigue threshold and growth properties of welded joints in a tensile residual stress field
|
Ohta, Akihiko |
|
1997 |
19 |
93 |
p. 303-310 8 p. |
artikel |