A study on the wake structure of an ascending submersible with silk flexible appendages using continuous wavelet transform and dynamic mode decomposition
Fei Yan,
No information about this author
G. Zhang,
No information about this author
Akira Rinoshika
No information about this author
et al.
Experimental Thermal and Fluid Science,
Journal Year:
2024,
Volume and Issue:
unknown, P. 111323 - 111323
Published: Sept. 1, 2024
Language: Английский
Four-dimensional particle tracking velocimetry measurements of unsteady three-dimensional vortex onset and progression for 5415 straight ahead, static drift, and pure sway
Physics of Fluids,
Journal Year:
2023,
Volume and Issue:
35(10)
Published: Oct. 1, 2023
Large-scale
towed
system
four-dimensional
particle
tracking
velocimetry
(4DPTV)
implementation
and
measurements
are
presented
for
towing
tank
tests
a
naval
combatant
5415
ship
model
straight
ahead,
static
drift
β
=
10°,
pure
sway
βmax
10°
conditions.
The
results,
the
first
time,
provide
instantaneous
volumetric
flow
field
data
around
including
near
hull
surface,
complete
description
of
sonar
dome
3D
unsteady
vortex
separation
onset
progression
due
to
4DPTV
larger
measurement
volume
higher
rates
in
comparison
with
previous
results
using
tomographic
image
(TPIV);
thereby,
providing
essential
required
assessment
current
hybrid
Reynolds-averaged
Navier–Stokes/large
eddy
simulation
turbulence
modeling
capabilities
guidance
necessary
improvements.
is
summarized
compared
TPIV,
camera
calibration
procedures,
trigger
systems,
synchronization
motion.
Analysis
reduction
procedures
core
detection
voxel
labeling
techniques,
described.
identification
complex
separations
breakdown
aided
complementary
detached
simulations.
vortex–vortex
interaction
process
visualized
from
datasets.
pros
cons
vs
between
second-
third-generation
visualization
technique,
statistical
convergence
error
analysis
port
discussed.
Plans
increased
spatial
resolution
additional
techniques
detailed
also
Language: Английский
FUN3D Mesh Adaptation Simulations for the 4th AIAA High-Lift Prediction Workshop Case 1a
Stephen L. Wood,
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Michael A. Park
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AIAA Aviation 2019 Forum,
Journal Year:
2022,
Volume and Issue:
unknown
Published: June 20, 2022
View
Video
Presentation:
https://doi.org/10.2514/6.2022-3394.vid
This
paper
describes
in
detail
the
FUN3D
Mesh
adaptation
simulation
results
for
Case
1a
of
4th
AIAA
High-Lift
Prediction
Workshop
(HLPW-4).
The
Stabilized
Finite
Element
library
with
is
used
along
Negative
Spalart-Allmaras
One-Equation
Model
to
simulate
fully
turbulent
free-air
flow
around
High
Lift
version
Common
Research
at
three
flap
settings.
Meshes
are
adapted
using
multi-scale
and
goal-oriented
metrics.
presented
discussion
focuses
on
predicted
differences
between
Coefficients
lift,
drag,
pitching
moment
within
7%
values
measured
QinetiQ
5m
Wind
Tunnel
each
setting.
Predicted
surface
pressures
skin
friction
distributions
show
inconsistent
discrepancies
measurements
across
Consequently,
increments
these
figures
merit
not
well
predicted.
These
predictions
consistent
submissions
HLPW-4
from
other
RANS-SA
methods.
Visualizations
Liutex
vortex
cores
colored
by
angular
velocity
as
possible
new
quantitative
qualitative
perspective
solution
evaluation.
Language: Английский
Numerical simulation of continuous bubbles motion behavior with different lance spacings
Xinting Tong,
No information about this author
Xiaohui Zhang,
No information about this author
Rui Feng
No information about this author
et al.
Thermal Science,
Journal Year:
2023,
Volume and Issue:
27(4 Part A), P. 2801 - 2811
Published: Jan. 1, 2023
The
lance
is
a
critical
component
of
the
bottom-blowing
pool
melting
process,
and
its
placement
has
an
important
impact
on
pool?s
gas-liquid
two-phase
flow.
In
this
study,
mathematical
model
process
established,
flow
pattern,
trajectory,
wake
vortex,
velocity
bubbles
under
four
spacings
are
simulated.
Results
show
that
there
three
basic
bubble
patterns
appear
in
field:
coalesce
before
leaving
nozzle
(Pattern
?),
after
no
coalescence
during
rise
III).
pattern
varies
from
Pattern
I
to
III
with
increase
spacing.
intensity
influence
vortex
decreases.
Q
(the
second
Galilean
invariant
gradient
tensor
?v)
value
small,
but
structural
distribution
complex.
Moreover,
large
difference
between
gas
liquid
at
beginning
injection,
them
decreases
so
average
turbulent
kinetic
energy
initially
increases
sharply,
then
approaches
dynamic
equilibrium.
top
bottom
velocities
consistent,
fluctuation
orderly.
greater
spacing
is,
disturbance
is.
mixing
effect
D
=
0.2
m
best
among
spacings.
Language: Английский