Risk Analysis of Fuel Leakage and Explosion in LNG-Powered Ship Cabin Based on Computational Fluid Dynamics
Fire,
Journal Year:
2025,
Volume and Issue:
8(5), P. 192 - 192
Published: May 10, 2025
In
order
to
analyze
the
explosion
risk
of
engine
room,
this
paper
uses
CFD
software
simulate
LNG
leakage
process
in
room
ship,
and
combustible
gas
cloud
obtained
from
simulation
explosion,
analyzing
its
combustion
dynamics.
On
basis
previous
studies,
studies
coupling
ensure
that
it
conforms
real
situation.
At
same
time,
taking
overpressure,
temperature,
mass
fraction
products
as
breakthrough
point,
harm
human
body
influence
ignition
source
location
on
propagation
characteristics
shock
wave
discusses
obstacles
diffusion
accumulation.
The
results
show
reaches
maximum
concentration
injection
direction,
cabin
have
a
significant
effect
accumulation
gas.
based
results,
can
be
determined
shape
pressure
field
generated
by
is
irregular,
at
obstacle
side
has
obvious
Finally,
reduce
hazard,
collaborative
strategy
modular
layout,
directional
ventilation,
detection
proposed,
which
provides
ideas
for
explosion-proof
design
cabin.
Language: Английский
Back-propagation oblique shock waves in turbine cascades induced by detonation
Yunying Qi,
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Hua Qiu,
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Cha Xiong
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et al.
Physics of Fluids,
Journal Year:
2025,
Volume and Issue:
37(5)
Published: May 1, 2025
The
interaction
mechanism
and
suppression
methods
between
the
backpropagation
oblique
shock
waves
(BOW)
from
detonation
combustion
in
afterburner
flow
disturbances
with
front-end
components,
remains
a
major
challenge
engine
coupling.
An
experimental
investigation
was
systematically
conducted
based
on
micro-axial
turbine.
evolution
characteristics
of
wave
system
structures
pressure
variations
turbine
field
under
influence
BOW
were
thoroughly
examined.
Special
emphasis
placed
modulation
effect
cascades
waves,
effectiveness
compared
different
equivalence
ratios.
results
indicate
that
complex
induced
within
cascade
channel
by
BOW,
significantly
enhancing
unsteady
field;
propagation
velocity
found
to
increase
ratio,
reaching
maximum
value
1818.18
m/s
at
an
ratio
1.4;
rotor
blades
exhibited
superior
stator,
drop
percentage
52.85%
for
cascade,
while
only
19.01%
achieved
stator
cascade.
This
study
provides
essential
evidence
theoretical
guidance
engines.
Language: Английский