Embed
Email

Explanation

Document Sample
Explanation
Shared by: HC111203211439
Categories
Tags
Stats
views:
3
posted:
12/3/2011
language:
Finnish
pages:
10
C:\Docstoc\Working\pdf\[322c1c0f-3d0c-4db1-baea-0beda9ced7c5.xls]Explanation







Look at the worksheet SGN420 - 337 ksi to understand these notes

This data sheet was done in ksi, to compare against provided graphs.



OVERVIEW

Data from Ford (& other databases) on fatigue expresses the fatigue-related properties

in terms of a set of coefficients. These are well explained in MSC-Fatigue notes.

We have linear analysis, want to account for non-linear behaviour. Hence need to use the Neuber

approximation to make an allowance for the fact that "real", plastic stresses will be lower than the ones

calculated in a linear FEA job.



The light-yellow shaded cells are the data input from these databases.

The light-brown shaded cells are user-selected values, to give sensible plot

ranges etc.



The data in columns L,M,N is just to plot the monotonic & cyclic Stress-strain curves,

based on the various input parameters supplied.



The strain-life plot is also built directly from the supplied input data (light green calculation cells)



All references state that it is not possible to go through the Neuber correction for plasticity

'directly': they state that this must be an iterative process. This may be true if we are starting from

the FE elastic analysis results, BUT these pages start from a choice of # cycles(N), or number of

reversals ( =2N).



Column F is doing the neuber calc via the 'iterative' process. Here, it's actually using a look up

table to give values of [stress*strain]. This is why - on this sheet only - columns L to Q are so long.

The method is to find the strs*strn (col O) corresponding to the total strain amplitude in col E

Then, having got this strs*strn value, we can derive the equivalent elastic stress (col G) simply

as stress = E*strn, so strs*strn * E = [strs*strs]elastic, so mult col F by E, root it to get elastic

equivalent stress (col G). This is not 100% accurate unless the look up table is very fine divisions,

but proves the method (see "Neuber S-N" plot in S-N curve)



Column H is finding the 'real' stress (as would be found in an elastic-plastic FE analysis) via a

look-up table, from the total strn ampl value in column E, looking for the same value in the cyclic

stress-strain table (col N), and simply seeing what ("real") stress it came from (column Q, only there

because the VLOOKUP function has to look in column 1, can't select it's value from a lower column than this)



Column I is a better way of getting the "real" (Plastic calc'd) stress. This relies on the fact that

the total strn ampl. Is made of separate elast & plast bits, so can easily find 'true' stress just by considering

it's elastic bit, FOR THIS life row.



Columns J,K do a similar thing for the Neuber stress. They rely on the fact that, for this chosen 'life' (e.g., row 11)

we know both the total strn ampl., and the real stress, so can get strs*strn directly, without the lookup method

of column F. Having got this, then getting the neuber stress (col K) from col J is as for getting col G from col F.

The text books don't explain how this can be done, BUT the values compare well, and actually agree better

with data as provided by landrover / dana (job 4059 / 4023).



The whole object of all this is to get S-N curves for the cases when we're working from FE calculated stresses.

On all other data sheets, which use the SI numbers, the blue shaded cells provide the S-N curves

to be used in GETSTR or similar. Use the top ones if the analysis was linear, the lower ones if the analysis

was a 'good', elasto-plastic job.



BEWARE everywhere the convention of using strain AMPLITUDE, but stress RANGE in the plots! Also

the use of REVERSALS in the X axes : the blue output data is in our (LSC) convention of stress amplitude vs cycles.



REFERENCES



MSC-fatigue on-line documentation, "Mscfatigue.pdf", Chap 14 [pages (approx) 1260+], esp equns 14-71

and 14-77

A B C D E F G H I J K L M N O P Q

1 C:\Docstoc\Working\pdf\[322c1c0f-3d0c-4db1-baea-0beda9ced7c5.xls]SGN420 - 337 ksi

2 1 ksi = 6.89E+00 Mpa

3 1298.00

4 sigF b ef c E K' n' K n

5 SI 649 -0.0816 0.104 -0.5657 155000 899 0.1442 480 0.1

6 ksi 94.1295 -0.0816 0.104 -0.5657 22480.85 130.4 0.1442 69.6 0.1

7

8

9 0.004187

Elas tot strn Cyc Neuber S- nom Monotoni Cyclic Elastic Nom

10 2Nf Ampl Plas Ampl Ampl. sts*strn N plastic Stress True SN neuber 2 stress c Cyclic Str.STrn Strn Stress

11 1 0.004187 0.104 0.108187 10.10588 953.2865 188 188.3 10.1836 956.945

12 10 0.00347 0.02827 0.03174 1.154346 322.1843 140 156.0 2.475925 471.8513

13 100 0.002875 0.007685 0.01056 0.435713 197.9415 120 129.3 0.682657 247.7636 0 0 0 0 0 0

14 1000 0.002383 0.002089 0.004472 0.176062 125.8258 100 107.1 0.239563 146.7729 1 4.45E-05 4.45E-05 4.45E-05 4.45E-05 1

15 10000 0.001975 0.000568 0.002543 0.109638 99.29244 88 88.8 0.112877 100.7485 2 8.9E-05 8.9E-05 0.000178 8.9E-05 2

16 1.00E+05 0.001636 0.000154 0.001791 0.062434 74.92874 72 73.6 0.065885 76.97126 3 0.000133 0.000133 0.0004 0.000133 3

17 1.00E+06 0.001356 4.2E-05 0.001398 0.04236 61.71821 60.8 61.0 0.042626 61.91166 4 0.000178 0.000178 0.000712 0.000178 4

18 5 0.000222 0.000222 0.001112 0.000222 5

19 6 0.000267 0.000267 0.001601 0.000267 6

20 7 0.000311 0.000311 0.00218 0.000311 7

21 Strain-Life 8 0.000356

S-N Curve 0.000356 0.002847 0.000356 8

22 9 0.0004 0.0004 0.003603 0.0004 9

23 10 0.000445 0.000445 0.004448 0.000445 10

24 0.1 1000 11 0.000489 0.000489 0.005383 0.000489 11

25 12 0.000534 0.000534 0.006406 0.000534 12

26 13 0.000578 0.000578 0.007519 0.000578 13

27 14 0.000623 0.000623 0.008721 0.000623 14

28 15 0.000667 0.000668 0.010013 0.000667 15

29 16 0.000712 0.000712 0.011395 0.000712 16

Stress RANGE (sig - R, ksi)

Strain AMPLITUDE









30 0.01 17 0.000757 0.000757 0.012868 0.000756 17

31 18 0.000802 0.000802 0.014432 0.000801 18

32 19 0.000847 0.000847 0.016088 0.000845 19

33 20 0.000893 0.000892 0.017838 0.00089 20

100

34 21 0.00094 0.000937 0.019683 0.000934 21

35 22 0.000989 0.000983 0.021626 0.000979 22

36 Plas Ampl 23 0.001039 0.001029 0.023668 0.001023 23

0.001

37 Elas Ampl 24 0.001091 0.001076 0.025814 0.001068

Neuber S-N 24

38 tot strn Ampl. 25 0.001148 0.001123 0.028066 0.001112 25

True SN

39 26 0.001209 0.00117 0.030432 0.001157 26

40 neuber 2 0.001278 0.001219 0.032916 0.001201

27 27

41 28 0.001357 0.001269 0.035526 0.001246 28

42 0.0001 29 0.001448 0.00132 0.03827 0.00129 29

43 1 10 100 1000 10000 100000 1000000 10 30 0.001556 0.001372 0.04116 0.001334 30

44 1.E+00 1.E+01 30.1

1.E+02 0.001568 0.001377 0.041458 0.001339

1.E+03 1.E+04 1.E+05 1.E+06 30.1

45 No. REVERSALS (2N) 30.2 0.00158 0.001383 0.041757 0.001343 30.2

No. REVERSALS (2N)

46 30.3 0.001592 0.001388 0.042058 0.001348 30.3

47 30.4 0.001605 0.001393 0.04236 0.001352 30.4

48 30.5 0.001618 0.001399 0.042664 0.001357 30.5

49 70 30.6 0.001631 0.001404 0.042969 0.001361 30.6

50 30.7 0.001644 0.00141 0.043277 0.001366 30.7

51 30.8 0.001658 0.001415 0.043585 0.00137 30.8

60

52 Cyclic 31 0.001686 0.001426 0.044208 0.001379 31

53 32 0.001846 0.001482 0.047429 0.001423 32

Monotonic

54 50 33 0.002042 0.001541 0.05084 0.001468 33

55 34 0.002286 0.001602 0.054462 0.001512 34

56 35 0.002591 0.001666 0.058318 0.001557 35

57 40 36 0.002972 0.001734 0.062434 0.001601 36

58 37 0.003449 0.001807 0.066844 0.001646 37

59 38 0.004044 0.001884 0.071582 0.00169 38

60 30 39 0.004787 0.001966 0.076689 0.001735 39

61 40 0.00571 0.002055 0.082212 0.001779 40

62 41 0.006856 0.002151 0.088205 0.001824 41

20

63 42 0.008272 0.002255 0.094727 0.001868 42

64 43 0.010015 0.002369 0.101846 0.001913 43

65 10

44 0.012153 0.002492 0.109638 0.001957 44

66 45 0.014767 0.002626 0.118188 0.002002 45

67 50 0.038835 0.003521 0.176062 0.002224 50

68 0 60 0.229353 0.007262 0.435713 0.002669 60

69 0 0.0025 0.005 0.0075 0.01 70 1.062094 0.016491 1.154346 0.003114 70

70 80 4.028944 0.037328 2.98621 0.003559 80

71 90 13.07572 0.080431 7.238817 0.004003 90

1000

72 91 14.60299 0.086563 7.877194 0.004048 91

73 92 16.28902 0.093104 8.56557 0.004092 92

900

74 93 18.14831 0.100078 9.30729 0.004137 93

75 800 Cyclic 94 20.1965 0.107509 10.10588 0.004181 94

76 Elastic Strn 95 22.45047 0.115422 10.96507 0.004226 95

77 700

96 24.9284 0.123841 11.88876 0.00427 96

78 97 27.64985 0.132795 12.88111 0.004315 97

79 600 98 30.63587 0.142311 13.94644 0.004359 98

80 100 37.49377 0.163146 16.31462 0.004448 100

81 500 125 349.1521 0.751364 93.92044 0.00556 125

82 150 2161.83 2.647447 397.1171 0.006672 150

83 400 175 10099.23 7.698998 1347.325 0.007784 175

84 200 38389.08 19.42482 3884.965 0.008896 200

85 300 225 124661.6 43.95317 9889.463 0.010009 225

86 250 357526.1 91.25651 22814.13 0.011121 250

87 200 275 927330.5 176.7224 48598.65 0.012233 275

88 300 2213707 323.0993 96929.78 0.013345 300

89 100 325 4928800 562.8568 182928.5 0.014457 325

90 350 10341607 940.998 329349.3 0.015569 350

91 0 375 20616754 1518.363 569386.1 0.016681 375

92 0 0.02 0.04 0.06 0.08 0.1 400 39310405 2375.462 950184.7 0.017793 400

93 425 72077034 3616.874 1537171 0.018905 425

94 450 1.28E+08 5376.252 2419313 0.020017 450

95 475 2.19E+08 7821.97 3715436 0.021129 475

96 500 3.66E+08 11163.45 5581725 0.022241 500

97 525 5.96E+08 15658.21 8220559 0.023353 525

98 550 9.5E+08 21619.65 11890806 0.024465 550

99 575 1.48E+09 29425.65 16919751 0.025577 575

100 600 2.27E+09 39528.01 23716809 0.026689 600

101 625 3.41E+09 52462.7 32789186 0.027801 625

102 650 5.05E+09 68861.04 44759677 0.028913 650

103 675 7.36E+09 89461.88 60386769 0.030026 675

104 700 1.06E+10 115124.6 80587247 0.031138 700

105 725 1.5E+10 146843.4 1.06E+08 0.03225 725

106 750 2.11E+10 185762.3 1.39E+08 0.033362 750

107 775 2.93E+10 233191.3 1.81E+08 0.034474 775

108 800 4.03E+10 290624 2.32E+08 0.035586 800

109 825 5.48E+10 359756 2.97E+08 0.036698 825

110 850 7.38E+10 442504.6 3.76E+08 0.03781 850

111 875 9.86E+10 541029.5 4.73E+08 0.038922 875

112 900 1.31E+11 657755.7 5.92E+08 0.040034 900

113 925 1.72E+11 795396.2 7.36E+08 0.041146 925

114 950 2.24E+11 956977.3 9.09E+08 0.042258 950

115 975 2.91E+11 1145865 1.12E+09 0.04337 975

116 1000 3.75E+11 1365791 1.37E+09 0.044482 1000

117 1025 4.8E+11 1620885 1.66E+09 0.045594 1025

118 1050 6.11E+11 1915703 2.01E+09 0.046706 1050

119 1075 7.73E+11 2255257 2.42E+09 0.047818 1075

120 1100 9.72E+11 2645055 2.91E+09 0.048931 1100

121 1125 1.22E+12 3091131 3.48E+09 0.050043 1125

122 1150 1.52E+12 3600082 4.14E+09 0.051155 1150

123 1175 1.88E+12 4179109 4.91E+09 0.052267 1175

124 1200 2.32E+12 4836057 5.8E+09 0.053379 1200

125 1225 2.85E+12 5579452 6.83E+09 0.054491 1225

126 1250 3.49E+12 6418552 8.02E+09 0.055603 1250

127 1275 4.26E+12 7363387 9.39E+09 0.056715 1275

128 1300 5.17E+12 8424809 1.1E+10 0.057827 1300

129 1325 6.25E+12 9614539 1.27E+10 0.058939 1325

130 1350 7.54E+12 10945221 1.48E+10 0.060051 1350

131 1375 9.06E+12 12430470 1.71E+10 0.061163 1375

132 1400 1.08E+13 14084934 1.97E+10 0.062275 1400

133 1425 1.29E+13 15924343 2.27E+10 0.063387 1425

134 1450 1.54E+13 17965575 2.61E+10 0.064499 1450

135 1475 1.83E+13 20226713 2.98E+10 0.065611 1475

136 1500 2.16E+13 22727107 3.41E+10 0.066723 1500

137 1525 2.55E+13 25487445 3.89E+10 0.067836 1525

138 1550 3E+13 28529814 4.42E+10 0.068948 1550

139 1575 3.52E+13 31877774 5.02E+10 0.07006 1575

140 1600 4.12E+13 35556427 5.69E+10 0.071172 1600

141 1625 4.81E+13 39592494 6.43E+10 0.072284 1625

142 1650 5.61E+13 44014389 7.26E+10 0.073396 1650

143 1675 6.52E+13 48852301 8.18E+10 0.074508 1675

144 1700 7.56E+13 54138269 9.2E+10 0.07562 1700

145 1725 8.75E+13 59906275 1.03E+11 0.076732 1725

146 1750 1.01E+14 66192321 1.16E+11 0.077844 1750

147 1775 1.16E+14 73034523 1.3E+11 0.078956 1775

148 1800 1.34E+14 80473201 1.45E+11 0.080068 1800

149 1825 1.54E+14 88550970 1.62E+11 0.08118 1825

150 1850 1.76E+14 97312843 1.8E+11 0.082292 1850

151 1875 2.01E+14 1.07E+08 2E+11 0.083404 1875

152 1900 2.3E+14 1.17E+08 2.22E+11 0.084516 1900

153 1925 2.62E+14 1.28E+08 2.47E+11

154 1950 2.98E+14 1.4E+08 2.73E+11

155 1975 3.39E+14 1.53E+08 3.02E+11

156 2000 3.84E+14 1.67E+08 3.34E+11

157 2025 4.35E+14 1.82E+08 3.69E+11

SI Units C:\Docstoc\Working\pdf\[322c1c0f-3d0c-4db1-baea-0beda9ced7c5.xls]SGN420 - 337 SI For GETSTR input

1 ksi = 6.89E+00 Mpa OUTPUTS NEUBER (to get 'ELAST-PLAST' from Elastic only analysis Damage Interpolator

INPUTS N (CYCLES) Stress AMPL

sigF b ef c E K'

n' K n 5.00E-01 3298.952 2000 2.551223982

SI 649 -0.0816 0.104 -0.5657 155000

899 0.1442 480 0.1 5.00E+00 1626.65 1000 28.45894555

ksi 94.1295 -0.0816 0.104 130.4

-0.5657 22480.85 0.1442 69.6 0.1 5.00E+01 854.1351 600 236.3026396

5.00E+02 505.9819 375.657 3093.924601

Choose these ranges to give sensible plots / results ranges 5.00E+03 347.3182 345.016 5292.675469

5.00E+04 265.3491 265.35 49998.15697

Elas Plas tot strn Stress* nom Monotoni

2Nf Ampl Ampl Ampl. True SN Strain Neuber stress c Cyclic 5.00E+05 213.4329 2006 2.43985E-06

1 0.004187 0.104 0.108187 1298.0 70.21343 6597.903 0 0 0 5.00E+06 175.0803 2007 0.001074617

10 0.00347 0.02827 0.03174 1075.7 17.0709 3253.299957 10 6.45E-05 6.45E-05 1.00E+03 445.185

100 0.002875 0.007685 0.01056 891.4 4.706753 1708.270143 20 0.000129 0.000129

1000 0.002383 0.002089 0.004472 738.7 1.651727 1011.963753 30 0.000194 0.000194 REAL' (to be used after Elast-Plast FE solution)

10000 0.001975 0.000568 0.002543 612.2 0.778258 694.636376 40 0.000258 0.000258 0.5 649

1.00E+05 0.001636 0.000154 0.001791 507.3 0.454259 530.6981503 50 0.000323 0.000323 5 537.8296

1.00E+06 0.001356 4.2E-05 0.001398 420.4 0.293894 426.8658266 60 0.000387 0.000387 50 445.7021

1.00E+07 0.001124 1.14E-05 0.001135 348.4 0.197762 350.1606961 70 0.000452 0.000452 500 369.3556

2.00E+03 0.002252 0.001411 0.003663 698.1 1.278643 890.3700589 80 0.000516 0.000516 5000 306.0869

90 0.000581 0.000581 50000 253.6557

100 0.000645 0.000645 500000 210.2058

110 0.00071 0.00071 5000000 174.1986

120 0.000775 0.000775 1000 349.0444

130 0.000841 0.00084

140 0.000908 0.000906

S-N Curve

Strain-Life 150 0.000977 0.000972

160 0.001049 0.001039

170 0.001128 0.001106

10000

0.1 180 0.001216 0.001176

190 0.00132 0.001247

200 0.001448 0.00132

210 0.001612 0.001397

220 0.001828 0.001477









Stress RANGE (sig - R, MPa)

230 0.002122 0.001562

Strain AMPLITUDE









0.01 240 0.002525 0.001654

250 0.003082 0.001753

260 0.003852 0.001861

270 0.004913 0.001981000

280 0.006369 0.002113

290 0.008351 0.002262

0.001 300 0.01103 0.00243

Plas Ampl 310 0.014624 0.002621 True SN

Elas Ampl 320 0.019406 0.002839 Neuber

330 0.025719 0.003088

tot strn Ampl.

340 0.03399 0.003373

350 0.044746 0.0037

360 0.058636 0.004075

0.0001 100

370 0.076451 0.0045071.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06

1 10 100 1000 10000 100000 1000000 380 0.099151 0.005002

390 0.127898 0.005569 No. REVERSALS (2N)

No. REVERSALS (2N)

400 0.164086 0.00622

410 0.209386 0.006964

420 0.265785 0.007814

550 Stress - Strain Curves

430 0.335642 0.008784

440 0.421743 0.009887

500

450 0.527364 0.01114

450 460 0.656348 0.012561

470 0.813184 0.014168

400 480 1.003097 0.015983

490 1.232152 0.018029

350 500 1.507364 0.020329

Cyclic

Stress (MPa)









300 Monotonic



250



200



150



100



50



0

0 0.0025 0.005 0.0075 0.01

Strain

SI Units

1 ksi = 6.89E+00 Mpa

INPUTS

sigF b ef c E K' n' K

SI 986.6113 -0.0892 0.5598 -0.7181 167222.3 843.73 0.0983

ksi 1.43E+02 -0.0892 0.5598 -0.7181 2.43E+04 1.22E+02 0.0983



Choose these ranges to give sensible plots / results ranges



tot strn Stress*

2Nf Elas Ampl Plas Ampl Ampl. True SN Strain Neuber

1 0.0059 0.5598 0.5657 1973.2 558.126 19321.60606

10 0.004805 0.107135 0.11194 1606.9 89.93548 7756.086121

100 0.003912 0.020504 0.024416 1308.5 15.97439 3268.806777

1000 0.003186 0.003924 0.00711 1065.6 3.788093 1591.795898

10000 0.002594 0.000751 0.003345 867.7 1.451457 985.324247

1.00E+05 0.002113 0.000144 0.002256 706.6 0.797224 730.2426371

1.00E+06 0.00172 2.75E-05 0.001748 575.4 0.502905 579.989681

1.00E+07 0.001401 5.26E-06 0.001406 468.6 0.329478 469.451195

2.00E+03 0.002995 0.002385 0.00538 1001.7 2.694706 1342.557264









Strain-Life





0.1

Strain AMPLITUDE









0.01

220

230

240

250

260

270

0.001

Plas Ampl 280

290

Elas Ampl

300

tot strn Ampl. 310

320

330

0.0001 340

1 10 100 1000 10000 100000 1000000 350

360

No. REVERSALS (2N)

370

380

390

400

410

420

Stress - Strain Curves

430

550

440

500 450

460

450 470

Cyclic 480

400

Monotonic 490

350 500

Stress (MPa)









300



250



200



150



100



50



0

0 0.0025 0.005 0.0075 0.01

Strain

For GETSTR input

OUTPUTS NEUBER (to get 'ELAST-PLAST' from Elastic only analysis)

Stress AMPL

N (CYCLES)

n 5.00E-01 9660.803

5.00E+00 3878.043

5.00E+01 1634.403

5.00E+02 795.8979

5.00E+03 492.6621

5.00E+04 365.1213

nom

stress Monotonic Cyclic 5.00E+05 289.9948

0 #DIV/0! 0 5.00E+06 234.7256

10 #DIV/0! 5.98E-05 1.00E+03 671.2786

20 #DIV/0! 0.00012

30 #DIV/0! 0.000179 REAL' (to be used after Elast-Plast FE solution)

40 #DIV/0! 0.000239 0.5 986.6113

50 #DIV/0! 0.000299 5 803.4264

60 #DIV/0! 0.000359 50 654.2535

70 #DIV/0! 0.000419 500 532.7778

80 #DIV/0! 0.000478 5000 433.8565

90 #DIV/0! 0.000538 50000 353.302

100 #DIV/0! 0.000598 500000 287.7041

110 #DIV/0! 0.000658 5000000 234.2859

120 #DIV/0! 0.000718 1000 500.8345

130 #DIV/0! 0.000777

140 #DIV/0! 0.000837

S-N Curve

150 #DIV/0! 0.000897

160 #DIV/0! 0.000957

170 #DIV/0! 0.001017

10000

180 #DIV/0! 0.001077

190 #DIV/0! 0.001136

200 #DIV/0! 0.001196

210 #DIV/0! 0.001257

220 #DIV/0! 0.001317

Stress RANGE (sig - R, MPa)









230 #DIV/0! 0.001377

240 #DIV/0! 0.001438

250 #DIV/0! 0.001499

260 #DIV/0! 0.001561

270 #DIV/0! 1000

0.001624

280 #DIV/0! 0.001688

290 #DIV/0! 0.001753

300 #DIV/0! 0.001821

310 #DIV/0! 0.001892 True SN

320 #DIV/0! 0.001966 Neuber

330 #DIV/0! 0.002045

340 #DIV/0! 0.00213

350 #DIV/0! 0.002223

360 #DIV/0! 0.002325

100

370 #DIV/0! 0.002441

1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06

380 #DIV/0! 0.002572

390 #DIV/0! 0.002722 No. REVERSALS (2N)

400 #DIV/0! 0.002896

000









410 #DIV/0! 0.0031

420 #DIV/0! 0.00334

430 #DIV/0! 0.003623

440 #DIV/0! 0.00396

450 #DIV/0! 0.004362

460 #DIV/0! 0.00484

470 #DIV/0! 0.005411

480 #DIV/0! 0.006092

490 #DIV/0! 0.006903

500 #DIV/0! 0.007869

stic only analysis)









1.E+06

SI Units C:\Docstoc\Working\pdf\[322c1c0f-3d0c-4db1-baea-0beda9ced7c5.xls]AL LM24 A380 For GETSTR input

1 ksi = 6.89E+00 Mpa EG-R-5/0013/02 AlSi9Cu3Fe OUTPUTS NEUBER (to get 'ELAST-PLAST' from Elastic only analysis Damage Interpolator

INPUTS N (CYCLES) Stress AMPL

sigF b ef c E K' n' K n 5.00E-01 3677.486 2000 1.620250472

SI 441.8 -0.0997 0.3732 -0.9754 80839 330.4 0.0525 5.00E+00 1115.589 1000 6.450429779

5.00E+01 415.0145 600 10.7281505

5.00E+02 239.0949 375.657 14.46777722

Choose these ranges to give sensible plots / results ranges 5.00E+03 178.2524 345.016 8.570465904

5.00E+04 140.3929 265.35 87.24942171

Elas Plas tot strn Stress* nom Monotoni

2Nf Ampl Ampl Ampl. True SN Strain Neuber stress c Cyclic 5.00E+05 111.4572 2006 1.31222E-07

1 0.005465 0.3732 0.378665 883.6 167.2943 7354.971695 0 #DIV/0! 0 5.00E+06 88.58021 2007 5.5932E-07

10 0.004344 0.039495 0.043839 702.4 15.39527 2231.177702 10 #DIV/0! 0.000124 1.00E+03 215.9697

100 0.003453 0.00418 0.007633 558.3 2.130619 830.0290977 20 #DIV/0! 0.000247

1000 0.002745 0.000442 0.003187 443.8 0.707163 478.1898182 30 #DIV/0! 0.000371 REAL' (to be used after Elast-Plast FE solution)

10000 0.002182 4.68E-05 0.002229 352.7 0.393052 356.5048267 40 #DIV/0! 0.000495 0.5 441.8

1.00E+05 0.001734 4.95E-06 0.001739 280.4 0.24382 280.7857787 50 #DIV/0! 0.000619 5 351.1767

1.00E+06 0.001378 5.24E-07 0.001379 222.9 0.153672 222.9144772 60 #DIV/0! 0.000742 50 279.1423

1.00E+07 0.001096 5.55E-08 0.001096 177.2 0.097063 177.1604202 70 #DIV/0! 0.000866 500 221.8839

2.00E+03 0.002561 0.000225 0.002786 414.1 0.576985 431.9393854 80 #DIV/0! 0.00099 5000 176.3704

90 #DIV/0! 0.001113 50000 140.1928

100 #DIV/0! 0.001237 500000 111.4361

110 #DIV/0! 0.001361 5000000 88.57797

120 #DIV/0! 0.001484 1000 207.068

130 #DIV/0! 0.001608

140 #DIV/0! 0.001732

S-N Curve

Strain-Life 150 #DIV/0! 0.001856

160 #DIV/0! 0.00198

170 #DIV/0! 0.002106

10000

0.1 180 #DIV/0! 0.002236

190 #DIV/0! 0.002377

200 #DIV/0! 0.002544

210 #DIV/0! 0.002776

220 #DIV/0! 0.003154









Stress RANGE (sig - R, MPa)

230 #DIV/0! 0.003853

Strain AMPLITUDE









0.01 240 #DIV/0! 0.005237

250 #DIV/0! 0.008028

260 #DIV/0! 0.013634

1000

270 #DIV/0! 0.024718

280 #DIV/0! 0.046202

290 #DIV/0! 0.086975

0.001 300 #DIV/0! 0.162766

Plas Ampl 310 #DIV/0! 0.30086 True SN

Elas Ampl 320 #DIV/0! 0.547744 Neuber

330 #DIV/0! 0.981272

tot strn Ampl.

340 #DIV/0! 1.72977

350 #DIV/0! 3.001586

360 #DIV/0! 5.130248

0.0001 100

370 #DIV/0! 8.6425741.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06

1 10 100 1000 10000 100000 1000000 380 #DIV/0! 14.36026

390 #DIV/0! 23.54971 No. REVERSALS (2N)

No. REVERSALS (2N)

400 #DIV/0! 38.14071

410 #DIV/0! 61.04254

420 #DIV/0! 96.59652

300 Stress - Strain Curves

430 #DIV/0! 151.2182

440 #DIV/0! 234.3013

450 #DIV/0! 359.4785

250 460 #DIV/0! 546.3693

470 #DIV/0! 822.9816

480 #DIV/0! 1228.991

200 490 #DIV/0! 1820.189

500 #DIV/0! 2674.474



150

Cyclic

Monotonic

100





50





0

0 0.002 0.004 0.006 0.008 0.01


Related docs
Other docs by HC111203211439
TATIL �DEVI
Views: 3  |  Downloads: 0
?????????????? ...
Views: 15  |  Downloads: 0
??????????
Views: 1  |  Downloads: 0
studentlistpharmacy
Views: 2  |  Downloads: 0
Sheet1
Views: 1  |  Downloads: 0
?????????????????????? ...
Views: 19  |  Downloads: 0
Defens
Views: 21  |  Downloads: 0
sungkro
Views: 7  |  Downloads: 0
By registering with docstoc.com you agree to our
privacy policy

You are almost ready to download!

You are almost ready to download!