openrocket/doc/techdoc/figures/aerodynamics/component-normal-forces.fig
2023-04-18 21:48:26 -05:00

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#FIG 3.2 Produced by xfig version 3.2.5
Landscape
Center
Metric
A4
100.00
Single
-2
1200 2
0 32 #616161
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 10572 5233 107 107 10572 5233 10678 5216
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 10572 5233 68 68 10572 5233 10639 5220
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 3806 4645 49 49 3806 4645 3855 4638
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 3806 4645 77 77 3806 4645 3882 4635
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 5241 4770 49 49 5241 4770 5290 4763
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 5241 4770 77 77 5241 4770 5317 4761
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 6227 4856 49 49 6227 4856 6276 4850
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 6227 4856 77 77 6227 4856 6303 4847
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 7931 5006 49 49 7931 5006 7979 4999
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 7931 5006 77 77 7931 5006 8007 4996
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 9634 5155 49 49 9634 5155 9683 5148
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 9634 5155 77 77 9634 5155 9710 5145
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 12100 5370 49 49 12100 5370 12148 5363
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 12100 5370 77 77 12100 5370 12176 5361
1 3 0 0 0 0 39 -1 20 0.000 1 6.1959 12951 5445 49 49 12951 5445 13000 5438
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 12951 5445 77 77 12951 5445 13027 5435
1 3 0 2 0 7 40 -1 20 0.000 1 6.1959 9094 5105 107 107 9094 5105 9200 5088
2 1 0 1 32 0 70 -1 -1 4.000 0 0 -1 1 0 2
0 0 1.00 120.00 180.00
2025 3600 14400 3600
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
12946 5487 13095 3784
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
5239 4768 5266 4454
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
6225 4854 6272 4316
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
7929 5003 7964 4600
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
9632 5152 9585 5690
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
12098 5368 12133 4965
2 3 0 0 0 0 39 -1 20 0.000 0 0 -1 0 0 6
9105 4998 9094 5105 9203 5116 9196 5058 9158 5015 9105 4998
2 3 0 0 0 0 39 -1 20 0.000 0 0 -1 0 0 6
9086 5214 9094 5105 8987 5097 8994 5149 9037 5202 9086 5214
2 1 0 3 0 0 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
10574 5235 10640 4473
2 1 1 1 0 0 50 -1 -1 4.000 0 0 -1 0 0 2
10574 5235 10485 6390
2 1 0 1 0 0 50 -1 -1 4.000 0 0 -1 1 1 2
1 1 1.00 60.00 120.00
1 1 1.00 60.00 120.00
9016 6002 10495 6131
2 1 0 2 0 0 50 -1 20 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
3804 4643 3840 4239
2 3 0 1 0 7 60 -1 20 0.000 0 0 -1 0 0 5
6623 4437 9313 4673 9234 5569 6545 5334 6623 4437
2 1 0 1 32 0 70 -1 -1 4.000 0 0 -1 1 0 2
0 0 1.00 120.00 180.00
2025 4275 14400 4275
2 1 0 1 32 0 70 -1 -1 4.000 0 0 -1 1 0 2
0 0 1.00 120.00 180.00
2025 5625 14400 5625
2 1 0 1 32 0 70 -1 -1 4.000 0 0 -1 1 0 2
0 0 1.00 120.00 180.00
2025 6300 14400 6300
2 3 0 1 0 7 60 -1 20 0.000 0 0 -1 0 0 5
9313 4673 10194 4930 10147 5468 9234 5569 9313 4673
2 3 0 1 0 7 60 -1 20 0.000 0 0 -1 0 0 5
5711 4538 6623 4437 6545 5334 5664 5076 5711 4538
2 3 0 1 0 7 60 -1 20 4.000 0 0 -1 0 0 5
4814 4460 5711 4538 5664 5076 4767 4998 4814 4460
2 1 0 1 32 7 70 -1 20 0.000 0 0 -1 0 0 2
2025 4950 4410 4950
2 1 1 1 0 0 50 -1 -1 4.000 0 0 -1 0 0 2
9080 5134 8986 6284
2 1 0 1 0 7 61 -1 20 0.000 0 0 -1 0 0 4
12388 5665 12762 6555 14107 6673 13733 5782
2 1 0 1 0 7 61 -1 20 0.000 0 0 -1 0 0 4
12435 5127 12958 4314 14303 4432 13780 5244
2 3 0 1 0 7 60 -1 20 4.000 0 0 -1 0 0 5
10194 4930 13780 5244 13733 5782 10147 5468 10194 4930
2 1 0 1 32 0 70 -1 -1 4.000 0 0 -1 1 0 2
0 0 1.00 120.00 180.00
7425 4950 14400 4950
3 0 0 1 0 7 60 -1 20 0.000 0 0 0 3
2101 4493 3245 4323 4814 4460
0.000 1.000 0.000
3 0 0 1 0 7 60 -1 20 0.000 0 0 0 3
2101 4493 3198 4861 4767 4998
0.000 1.000 0.000
4 1 0 50 -1 0 9 6.1959 4 135 555 9737 6020 Stability\001
4 1 0 50 -1 0 9 6.1959 4 135 435 9721 6199 margin\001
4 0 32 70 -1 0 12 0.0000 4 135 615 2070 4185 Airflow\001
4 1 0 50 -1 0 12 0.0000 4 135 270 8991 6485 CG\001
4 1 0 50 -1 0 12 0.0000 4 135 240 10480 6574 CP\001
4 0 -1 40 -1 0 10 0.0000 4 105 345 10710 4590 Total\001
4 0 -1 40 -1 0 10 0.0000 4 105 450 10710 4725 normal\001
4 0 -1 40 -1 0 10 0.0000 4 105 315 10710 4860 force\001
4 0 -1 40 -1 0 10 6.1959 4 105 615 3398 4806 Nose cone\001
4 0 -1 40 -1 0 10 6.1959 4 135 315 5047 4963 Body\001
4 0 -1 40 -1 0 10 6.1959 4 105 555 5899 5047 Shoulder\001
4 0 -1 40 -1 0 10 6.1959 4 135 315 7749 5225 Body\001
4 0 -1 40 -1 0 10 6.1959 4 105 510 9377 4990 Boattail\001
4 0 -1 40 -1 0 10 6.1959 4 135 315 11907 5556 Body\001
4 0 -1 40 -1 0 10 6.1959 4 105 270 12792 5646 Fins\001