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TEXSTAN

Institut für Thermodynamik der Luft- und Raumfahrt - Universität Stuttgart
Mechanical Engineering - The University of Texas at Austin

 McGraw-Hill logo
  • home | 
  • overview | 
  • modeling | 
  • boundary layer | 
  • pipe flow | 
  • turbine blade
  • input variables | 
  • glossary | 
  • external flows | 
  • internal flows | 
  • users

  • home
  • sitemap
  • terms of use
  • history
  • YOU - the user
  • thanks & links
  • research TEXSTAN
  • what's new

home

  • sitemap
  • terms of use
  • history
  • YOU - the user
  • thanks & links
  • research TEXSTAN
  • what's new

overview

  • geometry
  • setup and run TEXSTAN
  • transport equations
  • boundary conditions
  • boundary condition smoothness
  • initial conditions
  • fluid properties
  • units
  • numerical accuracy
  • diagnostics

modeling

  • mixing length model
  • one-equation model
  • two-equation model
  • turbulent Prandtl number
  • roughness
  • curvature
  • transition

boundary layer

  • construction of the dataset
  • computational results
  • output files

pipe flow

  • construction of the dataset
  • computational results
  • output files

turbine blade

  • construction of the dataset
  • computational results

input variables

glossary

external flows

  • Reynolds number
  • friction
  • heat transfer
  • mass transfer
  • integration control
  • initial profiles
  • output files

internal flows

  • Reynolds number
  • friction
  • heat transfer
  • integration control
  • initial profiles
  • output files

users

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