forked from ebranlard/welib
-
Notifications
You must be signed in to change notification settings - Fork 0
/
VortexHelix.py
87 lines (69 loc) · 2.84 KB
/
VortexHelix.py
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
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
import numpy as np
import matplotlib.pyplot as plt
# Local
from welib.vortilib.elements.VortexHelix import *
def Params(a=1/3,U0=10,Lambda=6,R=100,nB=3):
h = 2*np.pi*R*(1-a)/Lambda
CT = 4*a*(1-a)
Gamma = CT*np.pi*R*U0/(nB*Lambda) # NOTE assume aprime = 0, large tip-sped ratio
return a,U0,R,Lambda,nB,h,CT,Gamma
def main():
import matplotlib.pyplot as plt
# import warnings
# warnings.filterwarnings('error')
# --------------------------------------------------------------------------------}
# --- Radial survey on the lifting line
# --------------------------------------------------------------------------------{
a,U0,R,Lambda,nB,h,CT,Gamma_B=Params()
Gamma_tot = Gamma_B*nB
psi_blade = 0*np.pi/2
method = 'wrench'
bWT = True # Convention WT or Propeller
bSemi = True # infinite helix or at the rotor
vr = np.linspace(0.1,2,100)*R
Xcp = vr
Ycp = Xcp*0
Zcp = Xcp*0
Omega = U0*Lambda/R
fig,axes = plt.subplots(1, 2, sharey=False, figsize=(6.4,4.8)) # (6.4,4.8)
fig.subplots_adjust(left=0.12, right=0.95, top=0.91, bottom=0.11, hspace=0.20, wspace=0.39)
# --- Axial induction on the lifting line
ax = axes[0]
ax.plot([0,1],[-a,-a],'k--',label='Momentum T. (B=infty)',lw=3.5)
ax.plot([1,2],[ 0, 0],'k--',lw=3)
for nB in [1, 3, 10, 500]:
ur,ut,uz = vh_u(Xcp,Ycp,Zcp,Gamma_tot/nB,R,h,psih=psi_blade,nB=nB,bWT=bWT,method=method,bSemi=bSemi)
ax.plot(Xcp/R,uz/U0, label='B = {:d}'.format(nB))
ax.set_xlabel(r'$r/R$ [-]')
ax.set_ylabel(r'$u_z/U_0$ [-]')
ax.set_ylim([-2*a, 1/2*a])
ax.tick_params(direction='in')
#ax.legend()
# --- Tangential induction on the lifting line
ax = axes[1]
#ax.plot([0,1],[-a,-a],'k--',label='Momentum T. (B=infty)',lw=3)
ut_th_inf=np.zeros(vr.shape)
ut_th_inf[vr<R]=0
ut_th_inf[vr>R]=Gamma_tot/(2*np.pi*vr[vr>R])/2
ax.plot(vr/R,ut_th_inf,'k--',label='Vortex cylinder (B=infty)',lw=3.5)
for nB in [1, 3, 10, 500]:
ur,ut,uz = vh_u(Xcp,Ycp,Zcp,Gamma_tot/nB,R,h,psih=psi_blade,nB=nB,bWT=bWT,method=method,bSemi=bSemi)
ax.plot(vr/R,ut, label='B = {:d}'.format(nB))
#a,U0,R,Lambda,nB,h,CT,Gamma_B=Params(Lambda=0.1,nB=10)
#h=1000
#nB=10
#ur,ut,uz = vh_u(Xcp,Ycp,Zcp,Gamma_tot/nB,R,h,psih=psi_blade,nB=nB,bWT=bWT,method=method,bSemi=bSemi)
#ax.plot(vr/R,ut, label='B= {:d} - Lambda = {:.1f}'.format(nB,Lambda))
ax.set_xlabel('r/R [-]')
ax.set_ylabel(r'$u_t$ [m/s]')
ax.set_ylim([-1, 1])
ax.tick_params(direction='in')
ax.legend()
fig.suptitle('Vortilib - Vortex helix lifting line velocity')
if __name__ == '__main__':
main()
plt.show()
if __name__=="__export__":
main()
from welib.tools.repo import export_figs_callback
export_figs_callback(__file__)