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LC3_final.txt
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---------------
LC: Load Cases Task 2/LC3/LC3
---------------
---------------
RF against Strength Failure for the Skin
---------------
1 2.6212
2 2.5904
3 2.5955
4 2.6212
5 2.5892
6 2.6460
7 2.6316
8 2.5904
9 2.6381
10 2.6355
11 2.5904
12 2.6355
13 2.6355
14 2.5904
15 2.6355
16 2.6355
17 2.5904
18 2.6355
19 2.6355
20 2.5904
21 2.6355
22 2.6381
23 2.5904
24 2.6316
25 2.6460
26 2.5892
27 2.6212
28 2.5955
29 2.5904
30 2.6212
---------------
RF against Strength Failure for the Stringers
---------------
37 25.7157
38 27.1795
39 23.8309
40 23.9386
41 23.3480
42 24.0472
43 24.1238
44 24.1678
45 24.1788
46 24.1568
47 24.1568
48 24.1238
49 24.1678
50 24.1678
51 24.1678
52 24.1238
53 24.1568
54 24.1568
55 24.1788
56 24.1678
57 24.1238
58 24.0472
59 23.3480
60 23.9386
61 23.8309
62 27.1795
63 25.7157
64 NaN
---------------
Minimum RF in LC3: 2.5892
---------------
Average stresses in XX
---------------
0 -18.830000
1 -22.763333
2 -22.333333
3 -22.240000
4 -22.203333
5 -22.203333
6 -22.240000
7 -22.333333
8 -22.763333
9 -18.830000
---------------
Average stresses in YY
---------------
0 5.890667
1 5.890333
2 5.890667
3 5.890333
4 5.890333
5 5.890333
6 5.890333
7 5.890667
8 5.890333
9 5.890667
---------------
Average stresses in XY
---------------
0 116.866667
1 115.866667
2 115.800000
3 115.866667
4 115.866667
5 115.866667
6 115.866667
7 115.800000
8 115.866667
9 116.866667
---------------
Critical Biaxial Stress
---------------
sigma_x_crit
0 -234.263378
1 -225.924658
2 -226.670336
3 -226.833931
4 -226.899526
5 -226.899526
6 -226.833931
7 -226.670336
8 -225.924658
9 -234.263378
---------------
RF against Panel Buckling Biaxial
---------------
RF
0 12.4410
1 9.9249
2 10.1494
3 10.1994
4 10.2192
5 10.2192
6 10.1994
7 10.1494
8 9.9249
9 12.4410
---------------
K_biax
---------------
k_biax
0 5.2671
1 5.0796
2 5.0964
3 5.1001
4 5.1016
5 5.1016
6 5.1001
7 5.0964
8 5.0796
9 5.2671
---------------
Critical Shear Stress
---------------
sigma_xy_crit
0 257.271676
1 257.271676
2 257.271676
3 257.271676
4 257.271676
5 257.271676
6 257.271676
7 257.271676
8 257.271676
9 257.271676
---------------
K_shear
---------------
k_shear
0 5.7844
1 5.7844
2 5.7844
3 5.7844
4 5.7844
5 5.7844
6 5.7844
7 5.7844
8 5.7844
9 5.7844
---------------
RF against Panel Buckling in Shear
---------------
RF
0 2.2014
1 2.2204
2 2.2217
3 2.2204
4 2.2204
5 2.2204
6 2.2204
7 2.2217
8 2.2204
9 2.2014
---------------
RF against Panel Buckling Combined
---------------
RF
0 3.4876
1 3.2940
2 3.3209
3 3.3236
4 3.3257
5 3.3257
6 3.3236
7 3.3209
8 3.2940
9 3.4876
---------------
minimum RF against panel buckling in LC3: RF 3.294
dtype: float64
---------------
Average stresses in Axial Stringers
---------------
1 -20.783333
2 -22.293333
3 -21.940000
4 -21.950000
5 -21.930000
6 -21.950000
7 -21.940000
8 -22.293333
9 -20.783333
---------------
Average stresses Combined in Stringers
---------------
Combined Stress
1 -20.793358
2 -22.485063
3 -22.200652
4 -22.154261
5 -22.135514
6 -22.154261
7 -22.200652
8 -22.485063
9 -20.793358
---------------
I_total
---------------
86608.4859
---------------
Radius of Gyration
---------------
7.9129
---------------
RF against Column Panel Buckling
---------------
Combined Stress
1 5.8407
2 5.4012
3 5.4704
4 5.4819
5 5.4865
6 5.4819
7 5.4704
8 5.4012
9 5.8407
---------------
Minimum RF against Column Panel Buckling in LC3: Combined Stress 5.4012
dtype: float64
---------------
RF against Crippling
---------------
1 12.5594
2 12.3049
3 12.7138
4 12.7138
5 12.7370
6 12.7138
7 12.7138
8 12.3049
9 12.5594
---------------
Minimum RF against crippling in LC3: 12.3049