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Geodise Component

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Geodise Component CAD system. Aim provides robust parametric CAD models for CFD simulation; ... CFD (Fluent, Hydra) Cost estimation. IGES/STEP, CADfix ... – PowerPoint PPT presentation

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Title: Geodise Component


1
Geodise Component CAD system
Overview
Wenbin Song Email w.song_at_soton.ac.uk Geodise
Project, e-Science Centre School of Engineering
Sciences University of Southampton
  • Aim provides robust parametric CAD models for
    CFD simulation
  • Requirements for CAD models
  • Data flows and problem specific data definition
  • RR Negatively Scarfed Engine Intake

2
Geodise Component CAD system
  • Requirements for CAD model
  • Parametric ability to respond automatically to
    the latest parametric changes
  • Generic ability to produce different geometries
    from one model
  • Robust low rate of failure for
    combinations of parameters

3
Geodise Component CAD system
Dataflow in simulation
  • CADfix
  • Seamless geometry exchange is not effortless, but
    often problematic, usually requires repairs -
    solution is robust modelling in CAD systems, such
    as avoiding very short entities, etc.

4
Geodise Component CAD system
  • Availability of CAD system
  • Pro/Engineering (version 2001200 for Windows),
    running locally
  • Model data files for geometry creation
  • Model part file (defining the shape
    paramterization, input parameters, etc.)
  • Trail file (script file used to generate
    IGES/STEP file in batch mode)
  • Input file (text file containing name-value
    pairs)
  • Three files need to be in local working directory
    and and resulting IGES file is also stored in it
    and with the same name
  • MATLAB function proe_iges() running locally
    generates an IGES file based on input file
  • Transfer of IGES/STEP file for mesh generation
  • Use of gd_putfile to transfer geometry file and
    Gambit journal file onto remote server

5
Geodise Component CAD system
Application One Negatively Scarfed Engine Intake
(Rolls-Royce)
Problems definition maximize noise reduction
without (significant) loss aerodynamic
performance for all operating conditions.
Parameters Intake geometry is defined using
Pro/E by a list of parameters, parameters that
are expected to be used in optimisation are
listed below Scarf_angle 10 (degree), shown as
d1 (d190-scarf_angle) in the following
figure Top_radius 1243 (mm), shown as
d220 Bottom_radius 1390 (mm), shown as
d221 Side_radius 1430 (mm), not
shown Fanface_radius 1241 (mm), not
shown Fanface_axial_distance 1818.43 (mm),
shown as d2 Center offset 5 (mm), shown as d5
Figure (a) A3XX-100 (b) three dimensional shape
of negatively scarfed engine intake (c)
parameters of intake vertical layout.
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