Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag

Rising fuel cost has motivated increased fuel efficiency for freight trains. At cruising speed,the largest contributing factor to the fuel consumption is aerodynamic drag. As a result of stagnationand flow separation on and around lead and trailing cars, the first and last railcars experiencegreater...

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Main Author: Stucki, Chad Lamar
Format: Others
Published: BYU ScholarsArchive 2019
Subjects:
Online Access:https://scholarsarchive.byu.edu/etd/7478
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8478&context=etd
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spelling ndltd-BGMYU2-oai-scholarsarchive.byu.edu-etd-84782019-09-04T03:01:26Z Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag Stucki, Chad Lamar Rising fuel cost has motivated increased fuel efficiency for freight trains. At cruising speed,the largest contributing factor to the fuel consumption is aerodynamic drag. As a result of stagnationand flow separation on and around lead and trailing cars, the first and last railcars experiencegreater drag than intermediate cars. Accordingly, this work focused on reducing drag on lead locomotivesby designing and optimizing an add-on nose fairing that is feasible for industrial operation.The fairing shape design was performed via computational fluid dynamic (CFD) software.The simulations consisted of two in-line freight locomotives, a stretch of rails on a raised subgrade,a computational domain, and a unique fairing geometry that was attached to the lead locomotive ineach non-baseline case. Relative motion was simulated by fixing the train and translating the rails,subgrade, and ground at a constant velocity. An equivalent uniform inlet velocity was applied atzero degree yaw to simulate relative motion between the air and the train.Five fairing families-Fairing Families A-E (FFA-FFE)-are presented in this thesis.Multidimensional regressions are created for each family to approximate drag as a function ofthe design variables. Thus, railroad companies may choose an alternative fairing if the recommendedfairing does not meet their needs and still have a performance estimate. The regression forFFE is used as a surrogate model in a surrogate based optimization. Results from a wind tunneltest and from CFD are reported on an FFE geometry to validate the CFD model. The wind tunneltest predicts a nominal drag reduction of 16%, and the CFD model predicts a reduction of 17%.A qualitative analysis is performed on the simulations containing the baseline locomotive, the optimalfairings from FFA-FFC, and the hybrid child and parent geometries from FFA & FFC. Theanalysis reveals that optimal performance is achieved for a narrow geometry from FFC becausesuction behind the fairing is greatly reduced. Similarly, the analysis reveals that concave geometriesboost the flow over the top leading edge of the locomotive, thus eliminating a vortex upstreamof the windshields. As a result, concave geometries yield greater reductions in drag.The design variable definitions for each family were strategically selected to improve manufacturability,operational safety, and aerodynamic performance relative to the previous families.As a result, the optimal geometry from FFE is believed to most completely satisfy the constraintsof the design problem and should be given the most consideration for application in the railroadindustry. The CFD solution for this particular geometry suggests a nominal drag reduction of 17%on the lead locomotive in an industrial freight train. 2019-04-01T07:00:00Z text application/pdf https://scholarsarchive.byu.edu/etd/7478 https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8478&context=etd http://lib.byu.edu/about/copyright/ Theses and Dissertations BYU ScholarsArchive aerodynamics computational fluid dynamics surrogate based optimization wind tunnel testing freight locomotives railcars friction drag pressure drag fairing fuel efficiency
collection NDLTD
format Others
sources NDLTD
topic aerodynamics
computational fluid dynamics
surrogate based optimization
wind tunnel
testing
freight locomotives
railcars
friction drag
pressure drag
fairing
fuel efficiency
spellingShingle aerodynamics
computational fluid dynamics
surrogate based optimization
wind tunnel
testing
freight locomotives
railcars
friction drag
pressure drag
fairing
fuel efficiency
Stucki, Chad Lamar
Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
description Rising fuel cost has motivated increased fuel efficiency for freight trains. At cruising speed,the largest contributing factor to the fuel consumption is aerodynamic drag. As a result of stagnationand flow separation on and around lead and trailing cars, the first and last railcars experiencegreater drag than intermediate cars. Accordingly, this work focused on reducing drag on lead locomotivesby designing and optimizing an add-on nose fairing that is feasible for industrial operation.The fairing shape design was performed via computational fluid dynamic (CFD) software.The simulations consisted of two in-line freight locomotives, a stretch of rails on a raised subgrade,a computational domain, and a unique fairing geometry that was attached to the lead locomotive ineach non-baseline case. Relative motion was simulated by fixing the train and translating the rails,subgrade, and ground at a constant velocity. An equivalent uniform inlet velocity was applied atzero degree yaw to simulate relative motion between the air and the train.Five fairing families-Fairing Families A-E (FFA-FFE)-are presented in this thesis.Multidimensional regressions are created for each family to approximate drag as a function ofthe design variables. Thus, railroad companies may choose an alternative fairing if the recommendedfairing does not meet their needs and still have a performance estimate. The regression forFFE is used as a surrogate model in a surrogate based optimization. Results from a wind tunneltest and from CFD are reported on an FFE geometry to validate the CFD model. The wind tunneltest predicts a nominal drag reduction of 16%, and the CFD model predicts a reduction of 17%.A qualitative analysis is performed on the simulations containing the baseline locomotive, the optimalfairings from FFA-FFC, and the hybrid child and parent geometries from FFA & FFC. Theanalysis reveals that optimal performance is achieved for a narrow geometry from FFC becausesuction behind the fairing is greatly reduced. Similarly, the analysis reveals that concave geometriesboost the flow over the top leading edge of the locomotive, thus eliminating a vortex upstreamof the windshields. As a result, concave geometries yield greater reductions in drag.The design variable definitions for each family were strategically selected to improve manufacturability,operational safety, and aerodynamic performance relative to the previous families.As a result, the optimal geometry from FFE is believed to most completely satisfy the constraintsof the design problem and should be given the most consideration for application in the railroadindustry. The CFD solution for this particular geometry suggests a nominal drag reduction of 17%on the lead locomotive in an industrial freight train.
author Stucki, Chad Lamar
author_facet Stucki, Chad Lamar
author_sort Stucki, Chad Lamar
title Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
title_short Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
title_full Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
title_fullStr Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
title_full_unstemmed Aerodynamic Design Optimization of a Locomotive Nose Fairing for Reducing Drag
title_sort aerodynamic design optimization of a locomotive nose fairing for reducing drag
publisher BYU ScholarsArchive
publishDate 2019
url https://scholarsarchive.byu.edu/etd/7478
https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=8478&context=etd
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