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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Main Author: Sindhu Paramasivam
Other Authors: Jorg Uwe Schluter
Format: Theses and Dissertations
Language:English
Published: 2015
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Online Access:http://hdl.handle.net/10356/65439
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Institution: Nanyang Technological University
Language: English
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spelling 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
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering
spellingShingle 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