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Aerospace and Mechanical Engineering
waves
Commits
ca62dcef
Commit
ca62dcef
authored
5 years ago
by
AmauryBilocq
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Trial to find the stagnation point
parent
cdb4bd20
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1 merge request
!63
Amaury
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flow/viscous/solver.py
+9
-1
9 additions, 1 deletion
flow/viscous/solver.py
with
9 additions
and
1 deletion
flow/viscous/solver.py
+
9
−
1
View file @
ca62dcef
...
...
@@ -20,6 +20,14 @@ class Solver():
def
run
(
self
):
'''
Solve BLE
'''
# define tangential velocity in 2D
vt
=
self
.
v
[:,
0
]
+
self
.
v
[:,
1
]
# define stagnation point
stag
=
np
.
argmin
(
abs
(
self
.
v
[:,
1
]))
#define the stagnation point
print
'
Stag is
'
print
stag
print
len
(
self
.
boundary
.
nodes
)
print
'
--- I am a fake BL solver and I am setting dummy blowing velocities! ---
'
# 6th order fitting of delta_star for naca 0012 at alpha = 0, from XFoil
a
=
0.000054925976379640116
...
...
@@ -32,4 +40,4 @@ class Solver():
for
i
in
range
(
0
,
self
.
nE
):
x
=
0.5
*
(
self
.
boundary
.
groups
[
0
].
tag
.
elems
[
i
].
nodes
[
0
].
pos
.
x
[
0
]
+
self
.
boundary
.
groups
[
0
].
tag
.
elems
[
i
].
nodes
[
1
].
pos
.
x
[
0
])
# CAUTION: a positive velocity will result in a suction!
self
.
u
[
i
]
=
-
(
b
+
2
*
c
*
x
+
3
*
d
*
x
*
x
*
+
4
*
e
*
x
*
x
*
x
+
5
*
f
*
x
*
x
*
x
*
x
+
6
*
g
*
x
*
x
*
x
*
x
*
x
)
# ue = d(delta_star) / dx
self
.
u
[
i
]
=
-
(
b
+
2
*
c
*
x
+
3
*
d
*
x
*
x
+
4
*
e
*
x
*
x
*
x
+
5
*
f
*
x
*
x
*
x
*
x
+
6
*
g
*
x
*
x
*
x
*
x
*
x
)
# ue = d(delta_star) / dx
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Adrien Crovato
@acrovato
mentioned in commit
465d2d5d
·
4 years ago
mentioned in commit
465d2d5d
mentioned in commit 465d2d5d1e3bd5759c463e62373d393c72a90434
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