Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity
Aircraft wake vortices are major problems in many busy airports. In this thesis, such wake vortices in ground proximity are simulated using a set of in-house CFD codes for solving Navier-Stokes equations numerically using Large-eddy simulation. The simulations are performed with flat ground for d...
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sg-ntu-dr.10356-654392023-03-11T17:01:07Z Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity Sindhu Paramasivam Jorg Uwe Schluter School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering Aircraft wake vortices are major problems in many busy airports. In this thesis, such wake vortices in ground proximity are simulated using a set of in-house CFD codes for solving Navier-Stokes equations numerically using Large-eddy simulation. The simulations are performed with flat ground for different crosswind velocities and turbulence intensities. The parameters like circulation, lateral and vertical position of the vortex centre, radius of the core, vortex separation distance are investigated with the aid of necessary graphs. Lamb-Oseen vortex model is used to initiate the counter-rotating vortex pair in the computational domain. The vortex is initialised at a time step when the crosswind flow has reached the end of the domain so that the impact of background turbulence due to the crosswind is replicated. Crosswinds with low velocities are not sufficient enough to accelerate the decay and push the vortex out of the domain while a crosswind flow with higher velocities can initiate the vortex decay at earlier time and is capable of pushing the downwind vortex out of the domain. The plot of a~' versus velocity for downwind vortex at early times .varies linearly with a non-zero y-intercept while that of upwind vortex at later times can be approximated to a linear curve with slight deviations in low velocity regime. Vortex pair descents initially and then bounces back for all crosswind velocities. The bounce back is height is lesser for higher velocities of crosswind. The separation distance between the vortices is maintained same for all crosswind velocities at earlier times. Low turbulence intensities do not affect any of the vortex characteristics while higher turbulence intensities have slight effects on the large-scale turbulent structures formed. The effects of crosswind and turbulence intensity in the formation of secondary vortices and its interaction with the primary vortices are described in detail. Master of Science (Aerospace Engineering) 2015-09-22T06:32:02Z 2015-09-22T06:32:02Z 2014 2014 Thesis http://hdl.handle.net/10356/65439 en 108 p. application/pdf |
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DRNTU::Engineering::Aeronautical engineering Sindhu Paramasivam Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
description |
Aircraft wake vortices are major problems in many busy airports. In this thesis, such
wake vortices in ground proximity are simulated using a set of in-house CFD codes for
solving Navier-Stokes equations numerically using Large-eddy simulation. The
simulations are performed with flat ground for different crosswind velocities and
turbulence intensities. The parameters like circulation, lateral and vertical position of
the vortex centre, radius of the core, vortex separation distance are investigated with the
aid of necessary graphs.
Lamb-Oseen vortex model is used to initiate the counter-rotating vortex pair in the
computational domain. The vortex is initialised at a time step when the crosswind flow
has reached the end of the domain so that the impact of background turbulence due to
the crosswind is replicated.
Crosswinds with low velocities are not sufficient enough to accelerate the decay and
push the vortex out of the domain while a crosswind flow with higher velocities can
initiate the vortex decay at earlier time and is capable of pushing the downwind vortex
out of the domain. The plot of a~' versus velocity for downwind vortex at early times
.varies linearly with a non-zero y-intercept while that of upwind vortex at later times can
be approximated to a linear curve with slight deviations in low velocity regime. Vortex
pair descents initially and then bounces back for all crosswind velocities. The bounce
back is height is lesser for higher velocities of crosswind. The separation distance
between the vortices is maintained same for all crosswind velocities at earlier times.
Low turbulence intensities do not affect any of the vortex characteristics while higher
turbulence intensities have slight effects on the large-scale turbulent structures formed.
The effects of crosswind and turbulence intensity in the formation of secondary vortices
and its interaction with the primary vortices are described in detail. |
author2 |
Jorg Uwe Schluter |
author_facet |
Jorg Uwe Schluter Sindhu Paramasivam |
format |
Theses and Dissertations |
author |
Sindhu Paramasivam |
author_sort |
Sindhu Paramasivam |
title |
Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
title_short |
Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
title_full |
Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
title_fullStr |
Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
title_full_unstemmed |
Numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
title_sort |
numerical analysis of effects of crosswind and turbulence intensity on aircraft wake-vortex in ground proximity |
publishDate |
2015 |
url |
http://hdl.handle.net/10356/65439 |
_version_ |
1761781464565809152 |