Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations

Wake vortices pose a threat to a following aircraft, because they can induce a roll and compromise the safety of everyone on board. Caused by a difference in pressure between the upper and the lower part of the wings, these invisible flows of air are a major hazard and have to be avoided by separati...

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Main Author: Schroeder, Nataliya
Other Authors: Civil Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/40924
http://scholar.lib.vt.edu/theses/available/etd-02042011-134736/
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-409242020-09-29T05:47:58Z Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations Schroeder, Nataliya Civil Engineering Trani, Antonio A. Hobeika, Antoine G. Abbas, Montasir M. Wake Turbulence NextGen Wake envelope Wake encounter PDARS Aircraft Spacing Air Traffic Control Wake Vortex Capacity Wake vortices pose a threat to a following aircraft, because they can induce a roll and compromise the safety of everyone on board. Caused by a difference in pressure between the upper and the lower part of the wings, these invisible flows of air are a major hazard and have to be avoided by separating the aircraft at considerable distances. One of the known constraints in airport capacity for both departure and arrival operations is the large headway resulting from the wake spacing separation criteria. Reducing wake vortex separations to a safe level between successive aircraft can increase capacity in the National Airspace System (NAS) with corresponding savings in delay times. One of the main goals of the Wake Encounter Model (WEM) described in this thesis is to assess the outcome from future reduced separation criteria in the NAS. The model has been used to test probable encounters in todayâ s operations, and can also be used to test NextGen scenarios, such as Close Parallel Approaches and reduced in-trail separation flights. This thesis presents model enhancements to account for aircraft turning maneuvers, giving the wake a more realistic shape. Three major airspaces, New York, Southern California and Atlanta, were analyzed using the original and the enhanced WEM to determine if the enhanced model better represents the conditions in todayâ s operations. Additionally, some analysis on the wake lateral travel for closely spaced runways is presented in this thesis. Finally, some extension tools for post -analysis, such as animation tool and various graphs depicting the interactions between wake pairs were developed. Master of Science 2014-03-14T21:28:31Z 2014-03-14T21:28:31Z 2011-01-31 2011-02-04 2011-03-01 2011-03-01 Thesis etd-02042011-134736 http://hdl.handle.net/10919/40924 http://scholar.lib.vt.edu/theses/available/etd-02042011-134736/ Schroeder_NT_T_2011.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic Wake Turbulence
NextGen
Wake envelope
Wake encounter
PDARS
Aircraft Spacing
Air Traffic Control
Wake Vortex
Capacity
spellingShingle Wake Turbulence
NextGen
Wake envelope
Wake encounter
PDARS
Aircraft Spacing
Air Traffic Control
Wake Vortex
Capacity
Schroeder, Nataliya
Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
description Wake vortices pose a threat to a following aircraft, because they can induce a roll and compromise the safety of everyone on board. Caused by a difference in pressure between the upper and the lower part of the wings, these invisible flows of air are a major hazard and have to be avoided by separating the aircraft at considerable distances. One of the known constraints in airport capacity for both departure and arrival operations is the large headway resulting from the wake spacing separation criteria. Reducing wake vortex separations to a safe level between successive aircraft can increase capacity in the National Airspace System (NAS) with corresponding savings in delay times. One of the main goals of the Wake Encounter Model (WEM) described in this thesis is to assess the outcome from future reduced separation criteria in the NAS. The model has been used to test probable encounters in todayâ s operations, and can also be used to test NextGen scenarios, such as Close Parallel Approaches and reduced in-trail separation flights. This thesis presents model enhancements to account for aircraft turning maneuvers, giving the wake a more realistic shape. Three major airspaces, New York, Southern California and Atlanta, were analyzed using the original and the enhanced WEM to determine if the enhanced model better represents the conditions in todayâ s operations. Additionally, some analysis on the wake lateral travel for closely spaced runways is presented in this thesis. Finally, some extension tools for post -analysis, such as animation tool and various graphs depicting the interactions between wake pairs were developed. === Master of Science
author2 Civil Engineering
author_facet Civil Engineering
Schroeder, Nataliya
author Schroeder, Nataliya
author_sort Schroeder, Nataliya
title Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
title_short Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
title_full Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
title_fullStr Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
title_full_unstemmed Analysis of Potential Wake Turbulence Encounters in Current and NextGen Flight Operations
title_sort analysis of potential wake turbulence encounters in current and nextgen flight operations
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/40924
http://scholar.lib.vt.edu/theses/available/etd-02042011-134736/
work_keys_str_mv AT schroedernataliya analysisofpotentialwaketurbulenceencountersincurrentandnextgenflightoperations
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