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Numerical Investigation of High-Speed Droplet Impact Upon a Solid Surface
Numerical Investigation of High-Speed Droplet Impact Upon a Solid Surface
Numerical Investigation of High-Speed Droplet Impact Upon a Solid Surface

Detailed Information

자료유형  
 학위논문 서양
최종처리일시  
20260202103825
ISBN  
9798314875537
DDC  
621
저자명  
Burrell, Erin May.
서명/저자  
Numerical Investigation of High-Speed Droplet Impact Upon a Solid Surface
발행사항  
[Sl] : University of Michigan, 2025
발행사항  
Ann Arbor : ProQuest Dissertations & Theses, 2025
형태사항  
154 p
주기사항  
Source: Dissertations Abstracts International, Volume: 86-11, Section: B.
주기사항  
Advisor: Johnsen, Eric.
학위논문주기  
Thesis (Ph.D.)--University of Michigan, 2025.
초록/해제  
요약The impact of high-speed liquid droplets onto a solid surface plays an important role in a wide range of applications including cleaning of semiconductor devices, steam turbines, and supersonic/hypersonic flight. The mechanical loads experienced by high-speed projectiles from atmospheric droplet interactions are critical in assessing their performance and structural integrity. Droplet impact has been widely studied in the incompressible to weakly compressible regime. However, limited work has been conducted on the (highly) compressible regime. High-speed droplet impacts pose a complex multiphysics challenge due to intricate shock interactions, which make predicting surface stresses difficult. The mechanism responsible for generating maximum pressure at large impact speeds remains poorly understood. Most research on high-speed impacts has focused on single droplet impact, leaving the effects of multiple high-speed droplets largely unexplored. This thesis aims to enhance the current understanding high-speed (highly compressible) droplet impacts through numerical simulations. It seeks to determine the necessary resolution requirements for accurately modeling surface pressure, investigate the role of compressibility in predicting potential surface damage during single droplet impacts, and explore the interactions of multiple impacting droplets. To achieve this objective, high-fidelity numerical simulations of water droplets impacting a rigid wall at Mach numbers greater than 2 are conducted using a second-order accurate method with adaptive mesh refinement and a consistent, conservative Phase-Field approach.This thesis investigates the model parameters and resolution requirements necessary for performing simulations that accurately capture the physics of high-speed droplet impacts. Accurately predicting the pressure on a surface during impact requires precise modeling of the droplet's air/water interface. Innovative modeling techniques (Phase-Field model) provide control over the numerical interface thickness, necessitating the identification of the correct parameters governing this thickness. The interface thickness and resolution parameters significantly affect both the maximum surface pressure and its wall location. Thin interfaces clearly demonstrate that pressure is generated in a highly compressed air pocket. A balanced combination of resolution parameters and numerical interface thickness can accurately capture the physics while minimizing computational costs. Building on an understanding of the resolution parameters that enable accurate physics, this thesis then computationally explores the role of compressibility in identifying the mechanism that generates maximum wall pressure. It also examines how increasing droplet speeds intensify compressibility effects, thereby raising the likelihood of potential damage. Notably, the maximum wall pressures occur within an air pocket compressed by the incoming droplet. These pressures exceed those predicted by classical water-hammer theory. However, the center-point pressure aligns with a modified equation accounting for compressibility. From the surface pressure and material properties, the potential deformation can be deduced.Leveraging the understanding of single high-speed droplet impact, the thesis study explores how changes in droplet spacing and size ratio influence the wall pressures resulting from the impact of two Mach 4 cylindrical droplets on a rigid surface through numerical simulations. The collision of lateral jets from the droplets produces a pressure that is notably higher than single droplet impact, when the droplets are sufficiently close to each other.By employing numerical simulations with appropriate resolution/model parameters, the pressure exerted on a surface by high-speed droplet impacts can be accurately predicted. This accurate characterization of the surface pressures is critical to predicting mechanical loads/possible damage, with the potential to lead design improvements (enhanced performance/structural integrity) for a number of applications, ranging from supersonic/hypersonic flight to steam turbines.
일반주제명  
Mechanical engineering
일반주제명  
Physics
일반주제명  
Engineering
일반주제명  
Materials science
키워드  
Droplets
키워드  
Water-hammer
키워드  
Multiphase flows
키워드  
Shocks
키워드  
Phase-Field approach
기타저자  
University of Michigan Mechanical Engineering
기본자료저록  
Dissertations Abstracts International. 86-11B.
전자적 위치 및 접속  
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MARC

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■1001  ▼aBurrell,  Erin  May.
■24510▼aNumerical  Investigation  of  High-Speed  Droplet  Impact  Upon  a  Solid  Surface
■260    ▼a[Sl]▼bUniversity  of  Michigan▼c2025
■260  1▼aAnn  Arbor▼bProQuest  Dissertations  &  Theses▼c2025
■300    ▼a154  p
■500    ▼aSource:  Dissertations  Abstracts  International,  Volume:  86-11,  Section:  B.
■500    ▼aAdvisor:  Johnsen,  Eric.
■5021  ▼aThesis  (Ph.D.)--University  of  Michigan,  2025.
■520    ▼aThe  impact  of  high-speed  liquid  droplets  onto  a  solid  surface  plays  an  important  role  in  a  wide  range  of  applications  including  cleaning  of  semiconductor  devices,  steam  turbines,  and  supersonic/hypersonic  flight.  The  mechanical  loads  experienced  by  high-speed  projectiles  from  atmospheric  droplet  interactions  are  critical  in  assessing  their  performance  and  structural  integrity.  Droplet  impact  has  been  widely  studied  in  the  incompressible  to  weakly  compressible  regime.  However,  limited  work  has  been  conducted  on  the  (highly)  compressible  regime.  High-speed  droplet  impacts  pose  a  complex  multiphysics  challenge  due  to  intricate  shock  interactions,  which  make  predicting  surface  stresses  difficult.  The  mechanism  responsible  for  generating  maximum  pressure  at  large  impact  speeds  remains  poorly  understood.  Most  research  on  high-speed  impacts  has  focused  on  single  droplet  impact,  leaving  the  effects  of  multiple  high-speed  droplets  largely  unexplored. This  thesis  aims  to  enhance  the  current  understanding  high-speed  (highly  compressible)  droplet  impacts  through  numerical  simulations.  It  seeks  to  determine  the  necessary  resolution  requirements  for  accurately  modeling  surface  pressure,  investigate  the  role  of  compressibility  in  predicting  potential  surface  damage  during  single  droplet  impacts,  and  explore  the  interactions  of  multiple  impacting  droplets.  To  achieve  this  objective,  high-fidelity  numerical  simulations  of  water  droplets  impacting  a  rigid  wall  at  Mach  numbers  greater  than  2  are  conducted  using  a  second-order  accurate  method  with  adaptive  mesh  refinement  and  a  consistent,  conservative  Phase-Field  approach.This  thesis  investigates  the  model  parameters  and  resolution  requirements  necessary  for  performing  simulations  that  accurately  capture  the  physics  of  high-speed  droplet  impacts.  Accurately  predicting  the  pressure  on  a  surface  during  impact  requires  precise  modeling  of  the  droplet's  air/water  interface.  Innovative  modeling  techniques  (Phase-Field  model)  provide  control  over  the  numerical  interface  thickness,  necessitating  the  identification  of  the  correct  parameters  governing  this  thickness.  The  interface  thickness  and  resolution  parameters  significantly  affect  both  the  maximum  surface  pressure  and  its  wall  location.  Thin  interfaces  clearly  demonstrate  that  pressure  is  generated  in  a  highly  compressed  air  pocket.  A  balanced  combination  of  resolution  parameters  and  numerical  interface  thickness  can  accurately  capture  the  physics  while  minimizing  computational  costs. Building  on  an  understanding  of  the  resolution  parameters  that  enable  accurate  physics,  this  thesis  then  computationally  explores  the  role  of  compressibility  in  identifying  the  mechanism  that  generates  maximum  wall  pressure.  It  also  examines  how  increasing  droplet  speeds  intensify  compressibility  effects,  thereby  raising  the  likelihood  of  potential  damage.  Notably,  the  maximum  wall  pressures  occur  within  an  air  pocket  compressed  by  the  incoming  droplet.  These  pressures  exceed  those  predicted  by  classical  water-hammer  theory.  However,  the  center-point  pressure  aligns  with  a  modified  equation  accounting  for  compressibility.  From  the  surface  pressure  and  material  properties,  the  potential  deformation  can  be  deduced.Leveraging  the  understanding  of  single  high-speed  droplet  impact,  the  thesis  study  explores  how  changes  in  droplet  spacing  and  size  ratio  influence  the  wall  pressures  resulting  from  the  impact  of  two  Mach  4  cylindrical  droplets  on  a  rigid  surface  through  numerical  simulations.  The  collision  of  lateral  jets  from  the  droplets  produces  a  pressure  that  is  notably  higher  than  single  droplet  impact,  when  the  droplets  are  sufficiently  close  to  each  other.By  employing  numerical  simulations  with  appropriate  resolution/model  parameters,  the  pressure  exerted  on  a  surface  by  high-speed  droplet  impacts  can  be  accurately  predicted.  This  accurate  characterization  of  the  surface  pressures  is  critical  to  predicting  mechanical  loads/possible  damage,  with  the  potential  to  lead  design  improvements  (enhanced  performance/structural  integrity)  for  a  number  of  applications,  ranging  from  supersonic/hypersonic  flight  to  steam  turbines.
■590    ▼aSchool  code:  0127.
■650  4▼aMechanical  engineering
■650  4▼aPhysics
■650  4▼aEngineering
■650  4▼aMaterials  science
■653    ▼aDroplets
■653    ▼aWater-hammer
■653    ▼aMultiphase  flows
■653    ▼aShocks
■653    ▼aPhase-Field  approach
■690    ▼a0548
■690    ▼a0794
■690    ▼a0537
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■71020▼aUniversity  of  Michigan▼bMechanical  Engineering.
■7730  ▼tDissertations  Abstracts  International▼g86-11B.
■790    ▼a0127
■791    ▼aPh.D.
■792    ▼a2025
■793    ▼aEnglish
■85640▼uhttp://www.riss.kr/pdu/ddodLink.do?id=T17358277▼nKERIS▼z이  자료의  원문은  한국교육학술정보원에서  제공합니다.

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