Commit 36690732 authored by Søren Andersen's avatar Søren Andersen
Browse files

SJAN: Commit before splitting RKN in Flex to allow interaction with DTU servos

parent d4286bcf
Pipeline #17045 failed with stage
in 2 seconds
../../../../../../Flex5/pyFlex5/pyFlex5/examples/DTU10.vda
\ No newline at end of file
../../../../../../Flex5/pyFlex5/pyFlex5/examples/DTU10MW_Rwt.pro
\ No newline at end of file
../../../../../../Flex5/pyFlex5/pyFlex5/examples/DTU10MW_tower.tda
\ No newline at end of file
../../../../../../Flex5/pyFlex5/pyFlex5/examples/Fund_v02_h0.fda
\ No newline at end of file
sweep
**** Blade data ****
DTU10.vda Blade data filename, '-'= data below
**** Rotor + Nacelle ***
3 B (number of blades)
1.0 1.0 1.0 1.0 1.0 1.0 K_flap_fak K_edge_fak, pairs, blade 1..3 ||ndres hvis man vil ndre stivhed af vinger
1.0 1.0 1.0 M_fak, blade 1..3 ||ndres hvis man vil ndre stivhed af vinger
0 0 0 Pitch offset blade 1..B (deg)
0 X_rod (offset blade data x) (m) || Hvis frste punkt p vinge har radius=0, selvom det er en distance (x_rod) fra centrum
-2.5 5 coning tilt (deg, deg)
7.1 2.7 Znav Zrn (rotor overhang + pos. of shaft bend)
105520 0 Mnav Zgnav
2.0E5 2.0E5 325671 Ixnav Iynav Iznav
1.3E10 1.3E10 2.05E9 ? Kgax Kgay Ktors (shaft stiffness, DOF 14,15,28) ||Scale 2.67 i forhold til NREL5MW
1500.5 50.0 Igenerator Ngear
446034 2.69 2.75 Mkab Zgkab XKK2
7.33E6 7.33E6 4.1E6 Ixkab Iykab Izkab
3.6E9 1.0E10 Ktx KKy (yaw- and tilt stiffness)
30 20 0.0 CdARz CdARxy ZlatR aero drag of nav ||Cd*A i z,x,y retning og distance fra punkt R til krafts angrebspunkt, kun vigtigt i storm
30 105 2.0 CdAKz CdAKxy ZlatK aero drag of nacelle ||Cd*A i z,x,y retning og distance fra punkt K til krafts angrebspunkt, kun vigtigt i storm
.03 .03 .03 .03 .1 Damp. DOF 11,12 + 14,15 + shaft tors. (log.decr.)
**** tower data ****
DTU10MW_tower.tda Tower data filename, '-'= data below
**** foundation data ****
Fund_v02_h0.fda Foundation data filename, '-'= data below
**** operational data ****
1.29 9.81e-5 Ro g
1.005 0.7 1 1 Omega Tetap Generator-on/off ((1 = on, 0 = off)
180 0 Psi Yaw (rotorpos yawpos, deg,deg)
10.0 0.14 0 0 Vnav Vexp Vdir Vslope
0.0 0.8 0.5 Turb.intens (u), Rel.ti. (v) and (w) 0.12 0.8 0.5
..\Wind\vs88152.int 0 Turbulence-filename T-offset (u)
..\Wind\vs88153v.int 0 Turbulence-filename T-offset (v)
..\Wind\vs88154w.int 0 Turbulence-filename T-offset (w)
**** data for simulation ***
0 0 0 0 Blade-dof: 1F 2F 1K 2K, 1 = active, 0=stiff
0 0 1 0 0 1 DOF 11..15 + 28 (shafttors) 1=active, 0=stiff, DOF11=yaw
0 0 0 0 DOF 7..10 (twr: L1, L2, T1, T2) L = long., T=transv.
0 0 0 0 0 0 DOF 1..6 (foundat: Tx, Tz,Ry, Ty,Rz, Rx) (T=transl,R=rot)
0 0.02 180.0 Tstart dt Tmax
0 20 2 2 Printop Nprint Filop Nfil
1 0.11 0.05 40 10 4 Stall dClda dCldaS AlfS ALrund TauFak
1 1.0 Dynamisk wake (0/1) DynWTCfak
1.0 1.0 Towershadow-factor Cd-factor (twr)
*** data for generator, brake, pitch etc. ****
-Gendat.inf Generatordata filename, '-'= data below
-Brakedat.inf Brakedata filename, '-'= data below
-Pitchdat.inf Pitchdata filename, '-'= data below
-Yawdat.inf Yaw data filename, '-'= data below
-Contrdat,inf Controldata filename, '-'= data belov
0-Winddat.inf Winddata filename, '-'= data below, '0'=no data
-Initdat.inf Initdata filename, '-'= default values used
-Restart.rstF Restart filename, '-'= default values used -Restart.rstF
*** Inputdata for Flex5 generator version 2.1 ***
DTU10MWVS
10000 0.05 0.2 Pref (kW), tau_g (s) tau_set (s)
5.0 0.7 F0 (Hz), Ksi (-), 2.order bandpass RPM-filter
1800 D_gen (Nm/rpm) Generator damping
120 300 600 P_loss (kW) at 0%, 50%, 100% Pref
60 480 P_loss_mech Nref (mech. loss (kW) at RPM, gen. off)
*** Inputdata for Flex5 brake model version 2.0 ***
DTU10MW
52.3 Dynamic brake moment on generator shaft (kNm)
62.8 Static brake moment (kNm)
0.7 tau (s)
0.0 T-delay (s)
0.0 0.25 0.05 V (deg), R/V, K0/Ktors ( mainshaft play )
*** Inputdata for Flex5 pitch model version 1.2 ***
DTU 10MW pitch servo : "Blade pitch servo and generator models are not included in this controller and should be modeled separately, if they are to be included in the simulations."
6.3 0.8 OMres (rad/s) Ksi-rel (< 1) OMres=resonance frequency (rad/s)
*** Inputdata for Flex5 yaw model version 1.0 ***
DTU 10MW
1.0 0.2 Yaw-rate (deg/s) Yaw-tau (s)
*** Inputdata for Flex5 control system version 3.2 ***
DTU 10MW, variable speed
401.6 6800 N1, Pow1 (rpm, kW) point on cubic part of P(rpm) curve
300 480 N_min, N_max (rpm, rpm)
10000 Pmax (kW)
2000 6000 KI KP (Nm/s/rpm, Nm/rpm) const RPM control
0.4 0.7 F0 (Hz), Ksi (-) 2.order RPM-filter 0.2 0.7
0.045 0.20 0.0 KI KP KD (deg/s/rpm, deg/rpm, deg/rpm*s) 0.03 0.10 0
6.0 KK (deg) (reduction of gain as function of pitch) 6.0
90 10 Teta_max Pitchrate_max (deg,deg/s)
10 TauV (sec) (wind-averaging for minimum pitch)
9 No. of lines in table for Wind, minPitch, pow(init) (m/s,deg, kW)
4 2.58 200
5 1.80 600
6 0.79 1500
7 0.0 2500
8 0.0 3600
9 0.0 5100
10 0.0 6800
12 0.0 9800
13 0.0 10000
-0.2 2 10 TePstart TePstop TePsstop (deg/s)
0.05 Tsamp (sec) control system
*** Inputdata for deterministic wind, version 1.1 ***
NM80 test
94 N number of lines in interpolation table below
40 3 0 T Vnav Vdir (s, m/s, deg)
41 4 0
460 4 0
461 5 0
880 5 0
881 6 0
1300 6 0
1301 7 0
1720 7 0
1721 8 0
2140 8 0
2141 9 0
2560 9 0
2561 10 0
2980 10 0
2981 11 0
3400 11 0
3401 12 0
3820 12 0
3821 13 0
4240 13 0
4241 14 0
4660 14 0
4661 15 0
5080 15 0
5081 16 0
5500 16 0
5501 17 0
5920 17 0
5921 18 0
6340 18 0
6341 19 0
6760 19 0
6761 20 0
7180 20 0
7181 21 0
7600 21 0
7601 22 0
8020 22 0
8021 23 0
8440 23 0
8441 24 0
8860 24 0
8861 25 0
9280 25 0
9281 25 0
9700 25 0
9701 25 0
10120 25 0
10121 24 0
10540 24 0
10541 23 0
10960 23 0
10961 22 0
11380 22 0
11381 21 0
11800 21 0
11801 20 0
12220 20 0
12221 19 0
12640 19 0
12641 18 0
13060 18 0
13061 17 0
13480 17 0
13481 16 0
13900 16 0
13901 15 0
14320 15 0
14321 14 0
14740 14 0
14741 13 0
15160 13 0
15161 12 0
15580 12 0
15581 11 0
16000 11 0
16001 10 0
16420 10 0
16421 9 0
16840 9 0
16841 8 0
17260 8 0
17261 7 0
17680 7 0
17681 6 0
18100 6 0
18101 5 0
18520 5 0
18521 4 0
18940 4 0
18941 3 0
19360 3 0
19361 3 0
Sensor list : FLEX5, NM80 var. speed, 07.12.07
No gain offset corr. c Volt Unit Name Description ----------
1 1.0 0.0 0.00 1.0 (deg) PSI Rotorposition
2 1.0 0.0 0.00 1.0 (m/s) Vhub Wind speed
3 1.0 0.0 0.00 1.0 (deg) Tetap Pitch angle B1
4 1.0 0.0 0.00 1.0 (r/s) Omega Rotor speed
5 1.0 0.0 0.00 1.0 (RPM) OmGen Generator speed
6 1.0 0.0 0.00 1.0 (kW) P Power (el.)
7 1.0 0.0 0.00 1.0 (kNm) Mgen Gen moment
8 1.0 0.0 0.00 1.0 ( m ) GX1 Found. defl x
9 1.0 0.0 0.00 1.0 ( m ) GX2 Found. defl z
10 1.0 0.0 0.00 1.0 (rad) GX3 Found. defl rot y
11 1.0 0.0 0.00 1.0 ( m ) GX4 Found. defl y
12 1.0 0.0 0.00 1.0 (rad) GX5 Found. defl rot z
13 1.0 0.0 0.00 1.0 (rad) GX6 Found. defl rot x
14 1.0 0.0 0.00 1.0 ( m ) GX7 1 Tower mode L
15 1.0 0.0 0.00 1.0 (rad) GX8 2 Tower mode L
16 1.0 0.0 0.00 1.0 ( m ) GX9 1 Tower mode T
17 1.0 0.0 0.00 1.0 (rad) GX10 2 Tower mode T
18 1.0 0.0 0.00 1.0 (rad) GX11 Tower torsion
19 1.0 0.0 0.00 1.0 (rad) GX12 Tilt angle
20 1.0 0.0 0.00 1.0 (rad) GX14 Shaft bending x
21 1.0 0.0 0.00 1.0 (rad) GX15 Shaft bending y
22 1.0 0.0 0.00 1.0 (rad) GX28 Shaft torsion
23 1.0 0.0 0.00 1.0 (-) -
24 1.0 0.0 0.00 1.0 (-) -
25 1.0 0.0 0.00 1.0 (dg/s) Tetp Pitch rate B1
26 1.0 0.0 0.00 1.0 (kNm) Mbrak Brake moment
27 1.0 0.0 0.00 1.0 ( m ) GZ1 1. flap mode B1
28 1.0 0.0 0.00 1.0 ( m ) GZ2 2. flap mode B1
29 1.0 0.0 0.00 1.0 ( m ) GZ3 1. chord mode B1
30 1.0 0.0 0.00 1.0 ( m ) GZ4 2. chord mode B1
31 1.0 0.0 0.00 1.0 ( m ) UF1 Flapwise defl. B1
32 1.0 0.0 0.00 1.0 ( m ) UK1 Edgewise defl. B1
33 1.0 0.0 0.00 1.0 ( m ) UF2 Flapwise defl. B2
34 1.0 0.0 0.00 1.0 ( m ) UK2 Edgewise defl. B2
35 1.0 0.0 0.00 1.0 ( m ) UF3 Flapwise defl. B3
36 1.0 0.0 0.00 1.0 ( m ) UK3 Edgewise defl. B3
37 1.0 0.0 0.00 1.0 (kN) Fx1 Snit R= 2.80m B1
38 1.0 0.0 0.00 1.0 (kN) Fy1 Snit R= 2.80m B1
39 1.0 0.0 0.00 1.0 (kN) Fz1 Snit R= 2.80m B1
40 1.0 0.0 0.00 1.0 (kNm) Mx1 Pit M R= 2.80m B1
41 1.0 0.0 0.00 1.0 (kNm) -My1 Flap M R= 2.80m B1
42 1.0 0.0 0.00 1.0 (kNm) Mz1 Edge M R= 2.80m B1
43 1.0 0.0 0.00 1.0 (kN) Fx1 Snit R= 2.80m B2
44 1.0 0.0 0.00 1.0 (kN) Fy1 Snit R= 2.80m B2
45 1.0 0.0 0.00 1.0 (kN) Fz1 Snit R= 2.80m B2
46 1.0 0.0 0.00 1.0 (kNm) Mx1 Pit M R= 2.80m B2
47 1.0 0.0 0.00 1.0 (kNm) -My1 Flap M R= 2.80m B2
48 1.0 0.0 0.00 1.0 (kNm) Mz1 Edge M R= 2.80m B2
49 1.0 0.0 0.00 1.0 (kN) Fx1 Snit R= 2.80m B3
50 1.0 0.0 0.00 1.0 (kN) Fy1 Snit R= 2.80m B3
51 1.0 0.0 0.00 1.0 (kN) Fz1 Snit R= 2.80m B3
52 1.0 0.0 0.00 1.0 (kNm) Mx1 Pit M R= 2.80m B3
53 1.0 0.0 0.00 1.0 (kNm) -My1 Flap M R= 2.80m B3
54 1.0 0.0 0.00 1.0 (kNm) Mz1 Edge M R= 2.80m B3
55 1.0 0.0 0.00 1.0 (kN) FxR1 Shaft (R1-sys)
56 1.0 0.0 0.00 1.0 (kN) FyR1 Shaft (R1-sys)
57 1.0 0.0 0.00 1.0 (kN) FzR1 Shaft (R1-sys), Thrust
58 1.0 0.0 0.00 1.0 (kNm) MxR1 Shaft (R1-sys)
59 1.0 0.0 0.00 1.0 (kNm) MyR1 Shaft (R1-sys)
60 1.0 0.0 0.00 1.0 (kNm) MzR1 Shaft (R1-sys), Torque
61 1.0 0.0 0.00 1.0 (kN) FxN Shaft (N -sys)
62 1.0 0.0 0.00 1.0 (kN) FyN Shaft (N -sys)
63 1.0 0.0 0.00 1.0 (kN) FzN Shaft (N -sys), Thrust
64 1.0 0.0 0.00 1.0 (kNm) MxN Shaft (N -sys), Yaw
65 1.0 0.0 0.00 1.0 (kNm) MyN Shaft (N -sys), Tilt
66 1.0 0.0 0.00 1.0 (kNm) MzN Shaft (N -sys), Torque
67 1.0 0.0 0.00 1.0 (kN) FxK1 Nacelle (K1-sys)
68 1.0 0.0 0.00 1.0 (kN) FyK1 Nacelle (K1-sys)
69 1.0 0.0 0.00 1.0 (kN) FzK1 Nacelle (K1-sys)
70 1.0 0.0 0.00 1.0 (kNm) MxK1 Nacelle (K1-sys), Yaw
71 1.0 0.0 0.00 1.0 (kNm) MyK1 Nacelle (K1-sys), Tilt
72 1.0 0.0 0.00 1.0 (kNm) MzK1 Nacelle (K1-sys)
73 1.0 0.0 0.00 1.0 (kNm) MyK2 Nacelle bottom H=115.63m
74 1.0 0.0 0.00 1.0 (kNm) MzK2 Nacelle bottom H=115.63m
75 1.0 0.0 0.00 1.0 (kN) FxTt Hnav, H=119.00m
76 1.0 0.0 0.00 1.0 (kN) FyTt Hnav, H=119.00m
77 1.0 0.0 0.00 1.0 (kN) FzTt Hnav, H=119.00m
78 1.0 0.0 0.00 1.0 (kNm) MxTt Hnav, H=119.00m
79 1.0 0.0 0.00 1.0 (kNm) MyTt Hnav, H=119.00m
80 1.0 0.0 0.00 1.0 (kNm) MzTt Hnav, H=119.00m
81 1.0 0.0 0.00 1.0 (kNm) Myh1 Tower bending, H= 69.00m, L
82 1.0 0.0 0.00 1.0 (kNm) Mzh1 Tower bending, H= 69.00m, T
83 1.0 0.0 0.00 1.0 (kN) FxTb Tower bottom (T-sys)
84 1.0 0.0 0.00 1.0 (kN) FyTb Tower bottom (T-sys)
85 1.0 0.0 0.00 1.0 (kN) FzTb Tower bottom (T-sys)
86 1.0 0.0 0.00 1.0 (kNm) MxTb Tower bottom (T-sys)
87 1.0 0.0 0.00 1.0 (kNm) MyTb Tower bottom (T-sys)
88 1.0 0.0 0.00 1.0 (kNm) MzTb Tower bottom (T-sys)
89 1.0 0.0 0.00 1.0 (kN) Fx Ax F R= 2.80m B1
90 1.0 0.0 0.00 1.0 (kN) Fz Flap F R= 2.80m B1
91 1.0 0.0 0.00 1.0 (kNm) -My Flap M R= 2.80m B1
92 1.0 0.0 0.00 1.0 (kNm) Mz Edge M R= 2.80m B1
93 1.0 0.0 0.00 1.0 (kN) Fx Ax F R= 25.00m B1
94 1.0 0.0 0.00 1.0 (kN) Fz Flap F R= 25.00m B1
95 1.0 0.0 0.00 1.0 (kNm) -My Flap M R= 25.00m B1
96 1.0 0.0 0.00 1.0 (kNm) Mz Edge M R= 25.00m B1
97 1.0 0.0 0.00 1.0 (kN) Fx Ax F R= 50.00m B1
98 1.0 0.0 0.00 1.0 (kN) Fz Flap F R= 50.00m B1
99 1.0 0.0 0.00 1.0 (kNm) -My Flap M R= 50.00m B1
100 1.0 0.0 0.00 1.0 (kNm) Mz Edge M R= 50.00m B1
101 1.0 0.0 0.00 1.0 (kN) Fx Ax F R= 75.00m B1
102 1.0 0.0 0.00 1.0 (kN) Fz Flap F R= 75.00m B1
103 1.0 0.0 0.00 1.0 (kNm) -My Flap M R= 75.00m B1
104 1.0 0.0 0.00 1.0 (kNm) Mz Edge M R= 75.00m B1
105 1.0 0.0 0.00 1.0 (m/s) Vhubv Wind, v-component
106 1.0 0.0 0.00 1.0 (m/s) Vhubw Wind, w-component
107 1.0 0.0 0.00 1.0 (m/s) Vhubh Wind, tot. horizontal
108 1.0 0.0 0.00 1.0 (deg) Wdir Wind direction, hub
109 1.0 0.0 0.00 1.0 (m) YKF Nacelle Y position Fsys
110 1.0 0.0 0.00 1.0 (m) ZKF Nacelle Z position Fsys
111 1.0 0.0 0.00 1.0 (rad) 1zK Nacelle tilt
112 1.0 0.0 0.00 1.0 (rad) 1yK Nacelle roll
113 1.0 0.0 0.00 1.0 (m) Atip Tip dist to Twr center
114 1.0 0.0 0.00 1.0 (RPM) OmF Generator RPM, filtered
115 1.0 0.0 0.00 1.0 (kW) Pset Gen Power, setpoint
116 1.0 0.0 0.00 1.0 (deg) Tset Pitch setpoint
117 1.0 0.0 0.00 1.0 (m/s) Vmid Wind speed, averaged
118 1.0 0.0 0.00 1.0 (deg) Tmin Minimum Pitch angle
119 1.0 0.0 0.00 1.0 (RPM) OmF Generator RPM, filtered
120 1.0 0.0 0.00 1.0 (kW) Pset Gen Power, setpoint
121 1.0 0.0 0.00 1.0 (deg) Tset Pitch setpoint
122 1.0 0.0 0.00 1.0 (m/s) Vmid Wind speed, averaged
123 1.0 0.0 0.00 1.0 (deg) Tmin Minimum Pitch angle
Sensor list : FLEX5, NM80, local vars., 01.10.09
No gain offset corr. c Volt Unit Name Description ----------
1 1.0 0.0 0.00 1.0 (deg) PSI Rotorposition
2 1.0 0.0 0.00 1.0 (m/s) Vhub Wind speed
3 1.0 0.0 0.00 1.0 (deg) Tetap Pitch angle(B1)
4 1.0 0.0 0.00 1.0 (r/s) Omega Rotor speed
5 1.0 0.0 0.00 1.0 (RPM) OmGen Generator speed
6 1.0 0.0 0.00 1.0 (kW) P Power (el.)
7 1.0 0.0 0.00 1.0 (kNm) Mgen Gen moment
8 1.0 0.0 0.00 1.0 (m/s) 5UX x: 5.00 UX down
9 1.0 0.0 0.00 1.0 (m/s) 30UX x: 30.00 UX down
10 1.0 0.0 0.00 1.0 (m/s) 55UX x: 55.00 UX down
11 1.0 0.0 0.00 1.0 (m/s) 79UX x: 79.00 UX down
12 1.0 0.0 0.00 1.0 (m/s) 5UY x: 5.00 UY left
13 1.0 0.0 0.00 1.0 (m/s) 30UY x: 30.00 UY left
14 1.0 0.0 0.00 1.0 (m/s) 55UY x: 55.00 UY left
15 1.0 0.0 0.00 1.0 (m/s) 79UY x: 79.00 UY left
16 1.0 0.0 0.00 1.0 (m/s) 5UZ x: 5.00 UZ Streamwise
17 1.0 0.0 0.00 1.0 (m/s) 30UZ x: 30.00 UZ Streamwise
18 1.0 0.0 0.00 1.0 (m/s) 55UZ x: 55.00 UZ Streamwise
19 1.0 0.0 0.00 1.0 (m/s) 79UZ x: 79.00 UZ Streamwise
20 1.0 0.0 0.00 1.0 (m/s) 5Vs x: 5.00 VX Spanwise
21 1.0 0.0 0.00 1.0 (m/s) 30Vs x: 30.00 VX Spanwise
22 1.0 0.0 0.00 1.0 (m/s) 55Vs x: 55.00 VX Spanwise
23 1.0 0.0 0.00 1.0 (m/s) 79Vs x: 79.00 VX Spanwise
24 1.0 0.0 0.00 1.0 (m/s) 5Vt x: 5.00 V*COSTB Tangential
25 1.0 0.0 0.00 1.0 (m/s) 30Vt x: 30.00 V*COSTB Tangential
26 1.0 0.0 0.00 1.0 (m/s) 55Vt x: 55.00 V*COSTB Tangential
27 1.0 0.0 0.00 1.0 (m/s) 79Vt x: 79.00 V*COSTB Tangential
28 1.0 0.0 0.00 1.0 (m/s) 5Vn x: 5.00 V*SINTB Normal
29 1.0 0.0 0.00 1.0 (m/s) 30Vn x: 30.00 V*SINTB Normal
30 1.0 0.0 0.00 1.0 (m/s) 55Vn x: 55.00 V*SINTB Normal
31 1.0 0.0 0.00 1.0 (m/s) 79Vn x: 79.00 V*SINTB Normal
32 1.0 0.0 0.00 1.0 (deg) 5aoa x: 5.00 ACL aoa
33 1.0 0.0 0.00 1.0 (deg) 30aoa x: 30.00 ACL aoa
34 1.0 0.0 0.00 1.0 (deg) 55aoa x: 55.00 ACL aoa
35 1.0 0.0 0.00 1.0 (deg) 79aoa x: 79.00 ACL aoa
36 1.0 0.0 0.00 1.0 ( - ) 5CL x: 5.00 ACL CL
37 1.0 0.0 0.00 1.0 ( - ) 30CL x: 30.00 ACL CL
38 1.0 0.0 0.00 1.0 ( - ) 55CL x: 55.00 ACL CL
39 1.0 0.0 0.00 1.0 ( - ) 79CL x: 79.00 ACL CL
40 1.0 0.0 0.00 1.0 (1e6) 5Re x: 5.00 ACL Re
41 1.0 0.0 0.00 1.0 (1e6) 30Re x: 30.00 ACL Re
42 1.0 0.0 0.00 1.0 (1e6) 55Re x: 55.00 ACL Re
43 1.0 0.0 0.00 1.0 (1e6) 79Re x: 79.00 ACL Re
44 1.0 0.0 0.00 1.0 (N/m) 5PY x: 5.00 PY s-pitch
45 1.0 0.0 0.00 1.0 (N/m) 30PY x: 30.00 PY s-pitch
46 1.0 0.0 0.00 1.0 (N/m) 55PY x: 55.00 PY s-pitch
47 1.0 0.0 0.00 1.0 (N/m) 79PY x: 79.00 PY s-pitch
48 1.0 0.0 0.00 1.0 (N/m) 5PZ x: 5.00 PZ s-pitch
49 1.0 0.0 0.00 1.0 (N/m) 30PZ x: 30.00 PZ s-pitch
50 1.0 0.0 0.00 1.0 (N/m) 55PZ x: 55.00 PZ s-pitch
51 1.0 0.0 0.00 1.0 (N/m) 79PZ x: 79.00 PZ s-pitch
52 1.0 0.0 0.00 1.0 (N/m) 5PYr x: 5.00 PYr r-plan
53 1.0 0.0 0.00 1.0 (N/m) 30PYr x: 30.00 PYr r-plan
54 1.0 0.0 0.00 1.0 (N/m) 55PYr x: 55.00 PYr r-plan
55 1.0 0.0 0.00 1.0 (N/m) 79PYr x: 79.00 PYr r-plan
56 1.0 0.0 0.00 1.0 (N/m) 5PZr x: 5.00 PZr r-plans
57 1.0 0.0 0.00 1.0 (N/m) 30PZr x: 30.00 PZr r-plans
58 1.0 0.0 0.00 1.0 (N/m) 55PZr x: 55.00 PZr r-plans
59 1.0 0.0 0.00 1.0 (N/m) 79PZr x: 79.00 PZr r-plans
60 1.0 0.0 0.00 1.0 ( N ) 5SK1 x: 5.00 x-snitkraft
61 1.0 0.0 0.00 1.0 ( N ) 30SK1 x: 30.00 x-snitkraft
62 1.0 0.0 0.00 1.0 ( N ) 55SK1 x: 55.00 x-snitkraft
63 1.0 0.0 0.00 1.0 ( N ) 79SK1 x: 79.00 x-snitkraft
64 1.0 0.0 0.00 1.0 ( N ) 5SK2 x: 5.00 y-snitkraft
65 1.0 0.0 0.00 1.0 ( N ) 30SK2 x: 30.00 y-snitkraft
66 1.0 0.0 0.00 1.0 ( N ) 55SK2 x: 55.00 y-snitkraft
67 1.0 0.0 0.00 1.0 ( N ) 79SK2 x: 79.00 y-snitkraft
68 1.0 0.0 0.00 1.0 ( N ) 5SK3 x: 5.00 z-snitkraft
69 1.0 0.0 0.00 1.0 ( N ) 30SK3 x: 30.00 z-snitkraft
70 1.0 0.0 0.00 1.0 ( N ) 55SK3 x: 55.00 z-snitkraft
71 1.0 0.0 0.00 1.0 ( N ) 79SK3 x: 79.00 z-snitkraft
72 1.0 0.0 0.00 1.0 ( Nm) 5SK4 x: 5.00 x-snitmoment
73 1.0 0.0 0.00 1.0 ( Nm) 30SK4 x: 30.00 x-snitmoment
74 1.0 0.0 0.00 1.0 ( Nm) 55SK4 x: 55.00 x-snitmoment
75 1.0 0.0 0.00 1.0 ( Nm) 79SK4 x: 79.00 x-snitmoment
76 1.0 0.0 0.00 1.0 ( Nm) 5SK5 x: 5.00 y-snitmoment
77 1.0 0.0 0.00 1.0 ( Nm) 30SK5 x: 30.00 y-snitmoment
78 1.0 0.0 0.00 1.0 ( Nm) 55SK5 x: 55.00 y-snitmoment
79 1.0 0.0 0.00 1.0 ( Nm) 79SK5 x: 79.00 y-snitmoment
80 1.0 0.0 0.00 1.0 ( Nm) 5SK6 x: 5.00 z-snitmoment
81 1.0 0.0 0.00 1.0 ( Nm) 30SK6 x: 30.00 z-snitmoment
82 1.0 0.0 0.00 1.0 ( Nm) 55SK6 x: 55.00 z-snitmoment
83 1.0 0.0 0.00 1.0 ( Nm) 79SK6 x: 79.00 z-snitmoment
84 1.0 0.0 0.00 1.0 ( m ) 5UF x: 5.00 Flap Udboj
85 1.0 0.0 0.00 1.0 ( m ) 30UF x: 30.00 Flap Udboj
86 1.0 0.0 0.00 1.0 ( m ) 55UF x: 55.00 Flap Udboj
87 1.0 0.0 0.00 1.0 ( m ) 79UF x: 79.00 Flap Udboj
88 1.0 0.0 0.00 1.0 ( m ) 5UK x: 5.00 Kant Udboj
89 1.0 0.0 0.00 1.0 ( m ) 30UK x: 30.00 Kant Udboj
90 1.0 0.0 0.00 1.0 ( m ) 55UK x: 55.00 Kant Udboj
91 1.0 0.0 0.00 1.0 ( m ) 79UK x: 79.00 Kant Udboj
92 1.0 0.0 0.00 1.0 (N/m) 23TPy h: 23.00 Tower Py load
93 1.0 0.0 0.00 1.0 (N/m) 58TPy h: 57.50 Tower Py load
94 1.0 0.0 0.00 1.0 (N/m) 81TPy h: 80.50 Tower Py load
95 1.0 0.0 0.00 1.0 (N/m) **TPy h:115.63 Tower Py load
96 1.0 0.0 0.00 1.0 (N/m) 23TPz h: 23.00 Tower Pz load
97 1.0 0.0 0.00 1.0 (N/m) 58TPz h: 57.50 Tower Pz load
98 1.0 0.0 0.00 1.0 (N/m) 81TPz h: 80.50 Tower Pz load
99 1.0 0.0 0.00 1.0 (N/m) **TPz h:115.63 Tower Pz load
100 1.0 0.0 0.00 1.0 (kW) Paero Rotor Power
101 1.0 0.0 0.00 1.0 ( - ) Lambda Tip Speed Ratio
102 1.0 0.0 0.00 1.0 ( - ) CT Thrust Coeff
103 1.0 0.0 0.00 1.0 ( - ) CP Power Coeff(mech)
############################################################### ########### DTU COUPLER INPUT FILE ################# ###############################################################
# Global definition
cpltype = ["flx","dwc"] #["mir","haw"] #["mir"] #["haw"]
/mnt/mimer/sjan/git/hawc2cfd_pure/examples/launchcpl.py
\ No newline at end of file
========================================================================
Program Flex5, FORTRAN 90 Implementation, Version 01.01.2005
========================================================================
Following units are used as parts of the programme:
Flex5Glob : Version 01.01.2005
Flex5In : Version Flex5In 14.05.2003
Flex5Core : Version 17.11.2001
Flex5Tower: Tower model version 1.0, 20.05.2003
Flex5Fund : Foundation model version 2.0, 07.12.1999
Flex5Vind : Wind model version 1.1 e, 27.09.1993
Flex5Gen : Generator model ver. 2.1, (var. speed) 28.01.2008
Flex5Brak : Brake model version 2.0 e, 30.08.1994
Flex5Pitc : Pitch-servo version 1.2 e, (2. order respons) 14.10.1997
Flex5Yaw : Yaw-servo model version 1.0 e, 14.10.1997
Flex5Styr : Variable speed + pitch control, v.3.2e, 22.04.2008
Primary inputdata filename : Infile.pas Header : sweep
Resulting timeseries filename: sweep ID=15.10.2020 10:54
Blade data filename : DTU10.vda Text = DTU_10MW
Blade data used with X_root = 0.00 m (offset)
Structural data for blade (reference):
Station X (m) EI1 (Nm2) EI2 (Nm2) M (kg/m) FI (deg) Iud
1 2.80 6.18E+10 6.10E+10 1.19E+03 0.00 1
2 5.00 6.22E+10 6.11E+10 1.19E+03 0.00 0
3 10.00 5.45E+10 5.30E+10 1.11E+03 0.00 0
4 15.00 2.90E+10 3.84E+10 9.16E+02 0.00 0
5 20.00 1.56E+10 2.84E+10 7.91E+02 0.00 0
6 25.00 9.89E+09 2.15E+10 6.69E+02 0.00 1
7 30.00 6.47E+09 1.82E+10 5.87E+02 0.00 0
8 35.00 4.57E+09 1.44E+10 5.41E+02 0.00 0
9 40.00 3.23E+09 1.11E+10 4.90E+02 0.00 0
10 45.00 2.22E+09 8.31E+09 4.38E+02 0.00 0
11 50.00 1.50E+09 5.88E+09 3.83E+02 0.00 1
12 55.00 1.01E+09 4.00E+09 3.27E+02 0.00 0
13 60.00 6.81E+08 2.67E+09 2.75E+02 0.00 0
14 65.00 4.43E+08 1.71E+09 2.25E+02 0.00 0
15 70.00 2.68E+08 1.05E+09 1.76E+02 0.00 0
16 75.00 1.52E+08 6.09E+08 1.31E+02 0.00 1
17 79.00 8.63E+07 3.68E+08 9.67E+01 0.00 0
18 82.00 5.09E+07 2.45E+08 7.39E+01 0.00 0
19 85.00 2.23E+07 1.32E+08 4.96E+01 0.00 0
20 87.50 5.78E+06 5.03E+07 2.85E+01 0.00 0
21 89.17 1.02E+06 1.27E+07 1.54E+01 0.00 0
BETAC = 5.00 deg (structural pitch angle)
Blade geometry :
Station X (m) C (m) BETA (deg) T/C (pct) YAC/C
1 2.80 5.380 14.50 100.00 0.250
2 5.00 5.380 14.50 99.91 0.250
3 10.00 5.411 14.48 89.75 0.248
4 15.00 5.719 13.48 69.05 0.210
5 20.00 6.076 10.54 50.07 0.161
6 25.00 6.206 8.13 39.68 0.130
7 30.00 6.116 6.85 34.19 0.113
8 35.00 5.874 5.86 30.77 0.103
9 40.00 5.539 4.96 28.43 0.100
10 45.00 5.152 4.00 26.66 0.100
11 50.00 4.733 2.97 25.40 0.100
12 55.00 4.302 1.93 24.59 0.100
13 60.00 3.874 0.92 24.18 0.100
14 65.00 3.459 0.00 24.10 0.100
15 70.00 3.063 -0.82 24.10 0.100
16 75.00 2.690 -1.55 24.10 0.100
17 79.00 2.411 -2.12 24.10 0.100
18 82.00 2.190 -2.54 24.10 0.100
19 85.00 1.894 -2.95 24.10 0.100
20 87.50 1.483 -3.25 24.10 0.100
21 89.17 0.030 -3.43 24.10 0.100
X-tipbrake = 89.37 m (none)
Airfoil-data filename : DTU10MW_Rwt.pro
DTU
Airfoil no. 1 : FFA-W3-241 T/C = 24.00 %
Airfoil no. 2 : FFA-W3-301 T/C = 30.00 %
Airfoil no. 3 : FFA-W3-360 T/C = 36.00 %
Airfoil no. 4 : FFA-W3-"480" T/C = 48.00 %
Airfoil no. 5 : FFA-W3-"600" T/C = 60.00 %
Airfoil no. 6 : Cylinder T/C =100.00 %
Reference stiffness and mass values used with following correction factors:
Blade no. : 1 2 3
K_flap_fac : 1.000 1.000 1.000
K_edge_fac : 1.000 1.000 1.000
M_fac : 1.000 1.000 1.000
Pitch offset: 0.000 0.000 0.000 deg
Rotor and tower geometry :
B = 3 HNAV = 119.00 m
GAMMA = -2.50 deg D = 178.17 m
TILT = 5.00 deg ZNAV = 7.10 m
Hub and shaft data : Nacelle data :
MNAV = 1.06E+05 kg MKAB = 4.46E+05 kg
ZGNAV = 0.00E+00 m ZGKAB = 2.69E+00 m
IXNAV = 2.00E+05 kgm2 IXKAB = 7.33E+06 kgm2
IYNAV = 2.00E+05 kgm2 IYKAB = 7.33E+06 kgm2
IZNAV = 3.26E+05 kgm2 IZKAB = 4.10E+06 kgm2
KGAX = 1.30E+10 Nm/rad KTX = 3.60E+09 Nm/rad
KGAY = 1.30E+10 Nm/rad KKY = 1.00E+10 Nm/rad
KTORS = 2.05E+09 Nm/rad XKK2 = 2.75E+00 m
ZRN = 2.70E+00 m IGEN = 1.50E+03 kgm2
NGEAR = 5.00E+01
Tower data filename : DTU10MW_tower.tda , text = NREL
Foundation data filename : Fund_v02_h0.fda , text = Found.
Operational data : Data for simulation :
RO = 1.290 kg/m3 TSTART = 0.000 sec
G = 0.00 m/s2 DT = 0.0200 sec