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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2018
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Article
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Tab 10
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Research Article
Research on the Fatigue Performance of TC6 Compressor Blade under the CCF Effect
Table 10
HCF/LCF combined test records at different stress levels.
Serial number
Amplitude (
μ
m)
LCF load (N)
HCF load (MPa)
LCF life (cycle)
HCF life (cycle)
1
40
28,255
112.03
11,241
40,872,276
2
50
28,255
122.27
10,120
36,796,320
3
60
28,255
133.64
9400
34,178,400
4
70
28,255
141.59
8675
31,542,300
5
80
28,255
152.53
8094
29,429,784
6
90
28,255
166.28
7642
27,786,312
7
100
28,255
173.9
7270
26,433,720