openrocket/doc/techdoc/figures/aerodynamics/free-flight-forces.fig
2010-07-17 22:52:23 +00:00

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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
0 33 #9e9e9e
5 1 0 1 0 7 50 -1 -1 4.000 0 0 0 0 2797.454 2359.575 2815 1500 3008 1526 3160 1580
1 3 0 1 0 7 35 -1 20 0.000 1 6.1959 2636 3508 45 45 2636 3508 2681 3508
1 3 0 1 0 7 35 -1 20 0.000 1 6.1959 2583 3704 45 45 2583 3704 2628 3704
1 3 0 0 0 0 34 -1 20 2.000 1 0.0000 2584 3703 24 24 2584 3703 2603 3717
2 1 1 1 0 7 50 -1 -1 4.000 0 0 -1 0 0 2
2763 2048 2825 1336
2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
2521 1918 2384 3487
2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
3194 1977 3056 3546
2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
3866 2036 3729 3605
2 1 0 2 32 7 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
2635 3511 2775 1911
2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
1849 1860 1712 3429
2 1 0 2 0 7 40 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
2579 3699 3025 3827
2 3 0 0 0 0 34 -1 20 2.000 0 0 -1 0 0 6
2636 3467 2636 3508 2680 3508 2675 3489 2657 3469 2636 3467
2 1 1 1 0 7 50 -1 -1 4.000 0 0 -1 0 0 2
2481 4072 3211 1378
2 3 0 0 0 0 34 -1 20 2.000 0 0 -1 0 0 6
2636 3548 2636 3507 2592 3507 2597 3526 2615 3546 2636 3548
2 1 0 2 0 7 40 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
2583 3705 2502 4635
2 1 0 2 0 0 40 -1 -1 0.000 0 0 -1 1 0 2
0 0 2.00 60.00 120.00
2639 3517 2639 4260
2 1 0 1 0 7 55 -1 20 0.000 0 0 -1 0 0 4
2704 2731 2355 4036 2616 4105 2965 2802
2 1 2 1 0 7 60 -1 -1 1.000 0 0 -1 0 0 2
2638 1305 2638 5085
2 1 0 1 0 7 56 -1 20 0.000 0 0 -1 0 0 4
2685 3845 2837 3979 2766 4240 2616 4105
2 1 0 1 0 7 56 -1 20 0.000 0 0 -1 0 0 4
2424 3775 2228 3815 2157 4076 2355 4036
3 2 0 2 0 7 40 -1 -1 0.000 0 1 0 2
0 0 2.00 60.00 120.00
2216 5047 2478 4084
0.000 0.000
3 0 0 1 0 7 55 -1 20 0.000 0 0 0 5
2704 2731 2830 2439 2951 2332 3004 2486 2965 2802
0.000 1.000 1.000 1.000 0.000
4 0 0 50 -1 1 12 0.0000 4 135 135 3051 3920 N\001
4 0 0 50 -1 1 12 0.0000 4 135 135 2431 4797 D\001
4 0 0 50 -1 1 12 0.0000 4 135 105 2230 4502 T\001
4 0 0 50 -1 0 10 0.0000 4 105 195 2210 3718 CP\001
4 0 0 50 -1 0 10 0.0000 4 105 210 2252 3508 CG\001
4 0 33 50 -1 0 12 0.0000 4 135 615 1846 2181 Airflow\001
4 0 0 50 -1 32 12 0.0000 4 105 120 2952 1483 a\001
4 0 32 50 -1 1 12 0.0000 4 90 90 2835 2003 v\001
4 0 0 34 -1 1 12 0.0000 4 135 135 2651 4397 G\001