A Comprehensive investigation of volumetric heating Effects on supersonic nozzle flow patterns and condensation shocks, Considering Non-Equilibrium condensation and gas dynamics characteristics
Thermal Science and Engineering Progress,
Journal Year:
2025,
Volume and Issue:
59, P. 103331 - 103331
Published: Jan. 31, 2025
Language: Английский
Homogeneous–Heterogeneous condensation in supersonic nozzle using Eulerian–Eulerian approach: Numerical investigation of liquid phase modeling
Physics of Fluids,
Journal Year:
2025,
Volume and Issue:
37(2)
Published: Feb. 1, 2025
To
enhance
industrial
equipment,
it
is
crucial
to
have
a
thorough
understanding
of
the
occurring
phenomena
within
it.
Nonequilibrium
condensation
one
such
phenomenon
that
requires
comprehensive
investigation
and
study,
as
commonly
observed
in
equipment.
The
present
study
investigates
homogeneous
(HMC),
homogeneous–heterogeneous
(HMTC),
heterogeneous
(HTC)
through
implementation
liquid
droplet
injection
technique.
Two
contrasting
modeling
approaches
are
employed
for
analysis
HMTC.
In
Model
A,
discrete
simulation
performed
nucleating
injected
droplets,
with
each
group
modeled
independently.
B,
simplified
approach
employed,
where
radii
droplets
averaged
represent
combined
population.
results
demonstrate
HMC,
HMTC,
HTC
significantly
influence
flow
structure.
vapor
molecules
converging
nozzle
section
HMTC
elevated
pressure,
mass
fraction
(LMF),
temperature,
alongside
decrease
Mach
number
supersaturation
ratio.
scenario,
A
exhibits
higher
values
shock
intensity,
nucleation
rate,
number,
LMF,
two-phase
heat
compared
B.
When
comparing
outlet
average
LMF
difference
approximately
8%
Sample
1
6%
2.
Language: Английский
Design and optimization of slot number in supercooled vapor suction in steam turbine blades for reducing the wetness
Seyed Ali Hosseini,
No information about this author
Esmail Lakzian,
No information about this author
Daryoush Zarei
No information about this author
et al.
Energy,
Journal Year:
2024,
Volume and Issue:
301, P. 131633 - 131633
Published: May 19, 2024
Language: Английский
Numerical study of the impact of hot steam injection in the condensation flow through the low-pressure stage of steam turbine
Samaneh Masoumi,
No information about this author
Esmail Lakzian,
No information about this author
Heuy Dong Kim
No information about this author
et al.
Thermal Science and Engineering Progress,
Journal Year:
2024,
Volume and Issue:
53, P. 102698 - 102698
Published: June 13, 2024
Language: Английский
Steam condensing flow in cascade turbine blades and nozzles using simple low dissipation upwind scheme
Physics of Fluids,
Journal Year:
2025,
Volume and Issue:
37(3)
Published: March 1, 2025
In
various
engineering
applications,
the
phase
change
from
steam
to
water
droplet
during
rapid
expansion
under
supersonic
flow
conditions
is
inevitable.
The
occurrence
of
condensation
waves
due
latent
heat
released
and
aerodynamic
shocks
reduces
equipment
performance.
Given
complexities
two-phase
flow,
researchers
have
always
been
interested
in
developing
an
accurate
numerical
method
that
can
be
used
different
regimes
while
reducing
computation
costs.
This
research
has
developed
a
two-dimensional
code
using
simple
low-dissipation
advection
upstream
splitting
(SLAU)
high-resolution
(HR-SLAU)
complex
geometry
turbine
blades
convergent–divergent
nozzles.
performance
these
two
schemes
was
examined
Eulerian–Lagrangian
model
boundary
conditions.
governing
equations
are
investigated
Eulerian
model,
which
incorporates
SLAU
HR-SLAU
schemes,
for
determining
wet
parameters
solved
by
Lagrangian
approach
predict
liquid
mass
grid
cell.
Comparative
experimental
data,
regarding
simplicity
absence
any
tuning
flow-dependent
variable,
determination
position
intensity
improved
considerably,
radius
prediction
significantly
enhanced.
Notably,
scheme,
dissipation
component
pressure
flux
according
cell-interface
orientation
angle
characteristics
locally
controlled
coefficient
modeling
flows,
leads
fewer
errors.
Language: Английский
Progress in the research on non-equilibrium condensation of the compressor in the supercritical CO2 closed Brayton cycle system
Xinzhe Zhang,
No information about this author
Bin Yu,
No information about this author
Guoju Li
No information about this author
et al.
Physics of Fluids,
Journal Year:
2025,
Volume and Issue:
37(4)
Published: April 1, 2025
The
supercritical
carbon
dioxide
(S-CO2)
closed
Brayton
cycle
holds
significant
promise
for
revolutionizing
the
future
of
efficient
and
comprehensive
new
energy
utilization.
However,
compressor
operation
in
this
is
characterized
by
rapid
pressurization,
which
induces
substantial
fluctuations
temperature
pressure,
potentially
triggering
non-equilibrium
condensation
S-CO2.
This
phenomenon
disrupts
flow
field
within
compressor,
thereby
decreasing
overall
performance
system.
Therefore,
exploring
mechanism
great
significance
improving
work
summarizes
various
improvement
types
S-CO2
systems
engineering
applications
across
fields.
Subsequently,
it
reviews
development
theories
compressors,
focusing
on
nucleation
growth
models.
In
addition,
current
research
status
characteristics
under
high-speed
high-pressure
conditions
summarized,
based
convergent-divergent
nozzle
experiments
simulations.
systematically
progress
system
from
perspectives,
such
as
origin
technological
bottleneck,
nature
scientific
problem,
state
research.
By
reviewing
blade
humidity
control
method
condensation,
proposed
that
technology
active
multi-objective
coordination
should
be
direction
further
findings
analysis
can
provide
a
reference
design
blades
Language: Английский
Effects of intensity and location of volumetric cooling on non-equilibrium condensation in supersonic nozzle
International Communications in Heat and Mass Transfer,
Journal Year:
2025,
Volume and Issue:
165, P. 109054 - 109054
Published: May 8, 2025
Language: Английский
Prediction of condensation shock in supersonic nozzle: Comparison between high-pressure and low-pressure conditions at different of superheating degree
Yanyu Zhang,
No information about this author
Fengrong Liu,
No information about this author
Shanshan Liu
No information about this author
et al.
Chemical Engineering Science,
Journal Year:
2025,
Volume and Issue:
unknown, P. 121818 - 121818
Published: May 1, 2025
Language: Английский
Aerodynamic investigation and flow loss control on a newly designed leading edge fillet in a high-load turbine
Yue Li,
No information about this author
Weipeng Xue,
No information about this author
Lei Luo
No information about this author
et al.
Energy,
Journal Year:
2025,
Volume and Issue:
unknown, P. 136617 - 136617
Published: May 1, 2025
Language: Английский
Carbon dioxide separation from natural gas using a supersonic nozzle
Mahshid Mirzaie,
No information about this author
Esmail Lakzian,
No information about this author
Heuy Dong Kim
No information about this author
et al.
Physics of Fluids,
Journal Year:
2024,
Volume and Issue:
36(8)
Published: Aug. 1, 2024
Carbon
Dioxide
(CO2)
is
often
released
in
the
process
of
natural
gases
and
one
greenhouse
that
are
being
treated
as
most
troublesome
environmental
issues.
One
promising
ways
to
economically
remove
CO2
gas
processes
use
technology
supersonic
separation
makes
non-equilibrium
condensation
swirling
flows
convergent-divergent
nozzle
using
wet
outlet.
In
present
study,
mixture
Methane
(CH4)
was
considered
gas.
Two-dimensional
convergent–divergent
employed
produce
flow
with
condensation.
The
Peng–Robinson
real
model
used
for
A
nucleation
equation
a
droplet
growth
were
incorporated
into
governing
equations
compressible
Navier–Stokes
k-ω
turbulence
closure.
predicted
results
verified
validated
existing
experimental
data.
varied
investigate
its
effect
on
flow.
Technique
Order
Preference
by
Similarity
Ideal
Solution
method
applied
achieve
optimum
case
amounts
wetness
(the
mass
fraction
liquid
summation
vapor
at
outlet
nozzle)
kinetic
energy.
Three
locations
outlets
analyzed.
show
an
increase
divergent
angle
nozzle,
intensity,
inlet
supply
pressure
more
CO2.
However,
enhancement
mole
fractions
decreases
rate
wetness.
exit
from
increased
increasing
distance
throat.
Language: Английский