-
Notifications
You must be signed in to change notification settings - Fork 474
/
Copy pathad_blade_example.dat
30 lines (29 loc) · 4.23 KB
/
ad_blade_example.dat
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
------- AERODYN v15.04.* BLADE DEFINITION INPUT FILE -------------------------------------
Description line for this file -- file corresponds to inputs in Test01_UAE_AeroDyn.dat
====== Blade Properties =================================================================
23 NumBlNds - Number of blade nodes used in the analysis (-)
BlSpn BlCrvAC BlSwpAC BlCrvAng BlTwist BlChord BlAFID t_c BlCb BlCenBn BlCenBt BlCpn BlCpt BlCan BlCat BlCam
(m) (m) (m) (deg) (deg) (m) (-) (-) (-) (m) (m) (-) (-) (-) (-) (-)
0.0 0.0 0.0 0.0 0.000 0.219 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
0.1360 0.0 0.0 0.0 0.000 0.219 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
0.4481 0.0 0.0 0.0 -0.098 0.181 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
0.8001 0.0 0.0 0.0 19.423 0.714 3 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
1.0767 0.0 0.0 0.0 14.318 0.711 4 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
1.2779 0.0 0.0 0.0 10.971 0.691 5 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
1.4958 0.0 0.0 0.0 8.244 0.668 6 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
1.7137 0.0 0.0 0.0 6.164 0.647 7 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
1.9149 0.0 0.0 0.0 4.689 0.627 7 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.1160 0.0 0.0 0.0 3.499 0.606 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.3340 0.0 0.0 0.0 2.478 0.584 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.5520 0.0 0.0 0.0 1.686 0.561 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.7530 0.0 0.0 0.0 1.115 0.542 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
2.9542 0.0 0.0 0.0 0.666 0.522 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
3.1721 0.0 0.0 0.0 0.267 0.499 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
3.3900 0.0 0.0 0.0 -0.079 0.478 8 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
3.5912 0.0 0.0 0.0 -0.381 0.457 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
3.7924 0.0 0.0 0.0 -0.679 0.437 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
3.9684 0.0 0.0 0.0 -0.933 0.419 9 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
4.1444 0.0 0.0 0.0 -1.184 0.401 10 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
4.3456 0.0 0.0 0.0 -1.466 0.381 10 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
4.5216 0.0 0.0 0.0 -1.711 0.363 10 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0
4.5970 0.0 0.0 0.0 -1.711 0.363 10 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0