Moving doc/ to core/ directory.

[debian/openrocket] / core / doc / techdoc / figures / aerodynamics / free-flight-unstable.fig

diff --git a/core/doc/techdoc/figures/aerodynamics/free-flight-unstable.fig b/core/doc/techdoc/figures/aerodynamics/free-flight-unstable.fig
new file mode 100644 (file)
index 0000000..e31e9fb
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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 #c7c7c7
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+6 2157 2332 3004 4240
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+        2704 2731 2355 4036 2616 4105 2965 2802
+2 1 0 1 0 7 50 -1 -1 0.000 0 0 -1 0 0 4
+        2424 3775 2228 3815 2157 4076 2355 4036
+2 1 0 1 0 7 50 -1 -1 0.000 0 0 -1 0 0 4
+        2685 3845 2837 3979 2766 4240 2616 4105
+3 0 0 1 0 7 50 -1 -1 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
+-6
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+1 3 0 0 0 0 34 -1 20 2.000 1 0.0000 2634 3523 24 24 2634 3523 2653 3537
+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
+        2629 3519 3075 3647
+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
+        2633 3525 2552 4455
+4 0 0 50 -1 1 12 0.0000 4 135 135 3101 3740 N\001
+4 0 0 50 -1 1 12 0.0000 4 135 135 2481 4617 D\001
+-6
+6 2488 1664 2733 4743
+1 3 0 1 0 7 35 -1 20 0.000 1 6.1959 2544 3836 45 45 2544 3836 2589 3836
+2 1 1 1 0 7 50 -1 -1 4.000 0 0 -1 0 0 2
+        2671 2376 2733 1664
+2 1 0 2 32 7 50 -1 -1 0.000 0 0 -1 1 0 2
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+        2543 3839 2683 2239
+2 3 0 0 0 0 34 -1 20 2.000 0 0 -1 0 0 6
+        2544 3795 2544 3836 2588 3836 2583 3817 2565 3797 2544 3795
+2 3 0 0 0 0 34 -1 20 2.000 0 0 -1 0 0 6
+        2544 3876 2544 3835 2500 3835 2505 3854 2523 3874 2544 3876
+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
+        2547 3845 2547 4588
+4 0 32 50 -1 1 12 0.0000 4 90 90 2495 2370 v\001
+4 0 0 34 -1 1 12 0.0000 4 135 135 2526 4743 G\001
+-6
+2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
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+        2521 1918 2384 3487
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+        3194 1977 3056 3546
+2 1 0 1 33 7 50 -1 -1 0.000 0 0 -1 1 0 2
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+        3866 2036 3729 3605
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+       0 0 2.00 60.00 120.00
+        1849 1860 1712 3429
+2 1 1 1 0 7 50 -1 -1 4.000 0 0 -1 0 0 2
+        2481 4072 3211 1378
+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
+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