A Study of Particle Trajectories In A Gas Turbine Intake
An experimental and theoretical study of the particle trajectories in a gas turbine intake has been presented. computer model was written to simulate a particle behaviour flight in a theoretical flow which was assumed to inviscid, irrotational and incompressible. The model is also on other assumptio...
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Cranfield University
2010
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ndltd-CRANFIELD1-oai-dspace.lib.cranfield.ac.uk-1826-46222013-04-19T15:25:39ZA Study of Particle Trajectories In A Gas Turbine IntakeTan, S. C.An experimental and theoretical study of the particle trajectories in a gas turbine intake has been presented. computer model was written to simulate a particle behaviour flight in a theoretical flow which was assumed to inviscid, irrotational and incompressible. The model is also on other assumptions which imposes several limitations the accuracy of the predicted results. These limitations the objectives of the experimental investigation of particle trajectories which was carried out in a 30.0 section of an axisymmetric helicopter inertial separator. The separator section was fully instrumented with pressure tappings to determine the near-wall flow condition. The flowfield at the central (vertical) plane of separator was also measured with a two spot laser anemometer. The dust particles used in the tests were the spherical ballotini and irregular quartz particles with diameter ranging f-rom 15.0 to 150.0 microns. These particles seeded locally into the separator at three initial positions. The restitution ratios for the quartz particle based on experimental data and the ballotini particle's were based on a simple relation, which was derived by and error matching of predicted and experimental results. The particle trajectories, velocities and angles in separator were measured at several stations using the anemometer. The measured results were compared with predicted values from the model which has been modified accept both the experimentally measured and inviscid flowfield. The particle shape factor was also included to account for the higher drag on the non-spherical particle. Further modification was also made to include the restitution ratios of the ballotini particle. Good agreement found between measured and predicted particle trajecto- velocities and angles for both the spherical and non- spherical particle. The trajectories of the large particles (>100. Oum) are ballistic' in nature which are governed by the inertia forces. The trajectories of the smaller particles are influenced by the both aerodynamic and inertia forces.Cranfield UniversityElder, R. L.2010-10-28T11:36:34Z2010-10-28T11:36:34Z1988-01Thesis or dissertationDoctoralPhDhttp://dspace.lib.cranfield.ac.uk/handle/1826/4622en |
collection |
NDLTD |
language |
en |
sources |
NDLTD |
description |
An experimental and theoretical study of
the particle
trajectories in
a gas turbine intake has been
presented.
computer model was written to simulate a particle
behaviour
flight in
a
theoretical flow
which was assumed
to
inviscid, irrotational
and
incompressible. The model
is
also
on other assumptions which
imposes
several
limitations
the accuracy of the
predicted results. These limitations
the objectives of the
experimental
investigation of
particle
trajectories
which was carried out
in
a
30.0
section of an axisymmetric
helicopter inertial
separator. The separator section was fully instrumented with
pressure
tappings to determine the near-wall
flow
condition.
The flowfield
at the
central
(vertical) plane of
separator was also measured with a
two spot
laser
anemometer. The dust
particles used
in the tests were
the
spherical
ballotini
and
irregular
quartz particles with
diameter ranging
f-rom 15.0 to 150.0
microns. These particles
seeded
locally into the
separator at
three initial
positions.
The restitution ratios for the quartz particle
based on experimental
data
and the ballotini particle's
were
based
on a simple relation, which was
derived by
and error matching of predicted and experimental
results. The particle
trajectories,
velocities and angles
in
separator were measured at several stations using
the
anemometer.
The measured results were compared with
predicted values
from the model which
has been modified
accept
both the
experimentally measured and
inviscid
flowfield. The particle shape
factor
was also
included to
account
for the higher drag
on the non-spherical particle.
Further modification was also made
to include the
restitution ratios of the ballotini
particle.
Good agreement
found between measured and predicted particle
trajecto-
velocities and angles
for both the spherical and non-
spherical particle. The trajectories
of
the large particles
(>100. Oum)
are
ballistic' in
nature which are governed
by
the inertia forces. The trajectories
of the smaller particles
are
influenced by the both
aerodynamic and
inertia forces. |
author2 |
Elder, R. L. |
author_facet |
Elder, R. L. Tan, S. C. |
author |
Tan, S. C. |
spellingShingle |
Tan, S. C. A Study of Particle Trajectories In A Gas Turbine Intake |
author_sort |
Tan, S. C. |
title |
A Study of Particle Trajectories In A Gas Turbine Intake |
title_short |
A Study of Particle Trajectories In A Gas Turbine Intake |
title_full |
A Study of Particle Trajectories In A Gas Turbine Intake |
title_fullStr |
A Study of Particle Trajectories In A Gas Turbine Intake |
title_full_unstemmed |
A Study of Particle Trajectories In A Gas Turbine Intake |
title_sort |
study of particle trajectories in a gas turbine intake |
publisher |
Cranfield University |
publishDate |
2010 |
url |
http://dspace.lib.cranfield.ac.uk/handle/1826/4622 |
work_keys_str_mv |
AT tansc astudyofparticletrajectoriesinagasturbineintake AT tansc studyofparticletrajectoriesinagasturbineintake |
_version_ |
1716581481168502784 |