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CFD Exercises 1 Course : Aer E 311L Gas Dynamics Lab

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For the nozzle without plenum generated in previous exercise, set the boundary ... Outlet and plenum. Pressure (static) 101325 Pa. Temperature (static) 300 K ... – PowerPoint PPT presentation

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Title: CFD Exercises 1 Course : Aer E 311L Gas Dynamics Lab


1
CFD Exercises 1Course Aer E 311L Gas Dynamics
Lab
2
FLOWLAB - USAGE
  • Flowlab is installed in the windows labs. Go to
    Start -gt All Programs . Run Flowlab1.1.
  • This creates a file called Flowlab.ini in
    C\Documents and Settings\user. It looks as
    follows
  • FLOWLAB_WORK_DIR C\Temp\myflowlab
  • FLOWLAB_TEMPLATE_DIR z\Flowlab1.1\templates\nozz
    le
  • All your work is saved in FLOWLAB_WORK_DIR.
  • Remember to copy your final files to your home
    area in Clue or AFS.
  • Add AFS directory in the following way.
  • Start the AFS client.
  • Add \afs\iastate.edu\general\aero311l\Flowlab1.1\t
    emplates as F\
  • Define FLOWLAB_TEMPLATE_DIR to F\

3
FLOWLAB - GEOMETRY
  • Create a nozzle without plenum with the following
    dimensions
  • L1 .1016
  • L2 .0368
  • R1 .0128
  • R2 .0101
  • R3 .0114

4
FLOWLAB - PHYSICS
  • For the nozzle without plenum generated in
    previous exercise, set the boundary conditions in
    Flowlab by the following specifications. Choose
    inviscid model.
  • Inlet
  • Total pressure - 130000 Pa
  • Total temperature - 300 K
  • Outlet and plenum
  • Pressure (static) 101325 Pa
  • Temperature (static) 300 K

5
FLOWLAB - MESH
  • Continuing from the previous problem, create mesh
    using automatic-gtmedium option. The mesh should
    look like the following.

6
FLOWLAB SOLVE/REPORTS
  • Using the results for previous problems, and the
    default settings for converge criteria ( note the
    value ), solve.
  • Generate mach number plot at centerline.

7
FLOWLAB POST PROCESSING
  • Generate contour plots for density, pressure and
    mach number for the nozzle.

Contour plot for mach number.
8
FLOWLAB SUGGESTIONS
  • The display for the residual (XY plot) does not
    refresh properly if a new run is submitted after
    a previous run in the same section.
  • Workaround Start a new session.
  • Try to save your work as often as possible.
  • Most of the defaults are set to the nozzle
    dimension in the experiment. Use them.
  • If the pressure ratio is low, and the
    computational domain is large, there are
    convergence problems. So when having convergence
    problems, go for a small domain.
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