Fatigue Properties of Plain Concrete under Triaxial Tension-Compression-Compression Cyclic Loading
Table 2
Test data of fatigue for variable amplitude.
Specimen number
Fatigue life
Specimen number
Fatigue life
25250101
52203
24
0.45
215
25250301
52203
1004
121
1.79
255
25250102
52203
308
3.48
234
25250302
52203
1004
75
1.30
248
25250103
52203
272
3.09
238
25250303
52203
1004
13
0.64
192
25250104
52203
43
0.66
247
25250304
52203
1004
360
4.33
244
25250105
52203
640
7.01
204
25250305
52203
1004
29
0.81
232
25250201
19
816980
3.33
217
25250401
19
1004
1498232
6.24
234
25250202
19
185321
0.91
213
25250402
19
1004
300168
1.65
229
25250203
19
114847
0.64
225
25250403
19
1004
70474
0.77
203
25250204
19
91356
0.55
199
25250404
19
1004
49593
0.69
237
25250205
19
1934129
7.61
243
25250405
19
1004
109627
0.92
226
25500101
304705
110
1.86
327
25500301
304705
1060
67
1.52
308
25500102
304705
17
0.45
319
25500302
304705
1060
315
5.27
314
25500103
304705
43
0.85
313
25500303
304705
1060
16
0.74
301
25500104
304705
233
3.73
306
25500304
304705
1060
32
0.99
335
25500105
304705
59
1.09
286
25500305
304705
1060
143
2.67
327
25500201
13
2559519
1.88
310
25500401
13
1060
594174
0.89
334
25500202
13
700821
0.66
302
25500402
13
1060
1218818
130
305
25500203
13
594174
0.59
275
25500403
13
1060
289469
0.69
307
25500204
13
1767287
1.36
293
25500404
13
1060
319940
0.71
320
25500205
13
>2500000
>1.88
319
25500405
13
1060
>2500000
>2.14
261
50500101
17171
1057
2.08
ā
50500201
112
ā
340844
4.17
400
Note. , is the ultimate strain of specimen damage. Specimen numbering methods xxyyzztt: xxyy means the two directions of lateral compressive stress ratio, where 2550 indicates that one direction of lateral compressive stress ratio is 0.25, another is 0.50; zz represents the amplitude loading condition; 01, 02, 03, and 04 are four testing loading conditions for low-high, high-low, low-medium-high, and high-medium-low, respectively; tt represents the sample number to each operating mode.