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Flat layout & secundary drawings
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Flat layout
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3 D Contour &Vector  (xyz-c-uvw) projection plots
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Quasi 3D  & secundary drawings
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2 D line and symbol (xy) plots

2D vector drawing mode demos

Drawings  of  sectional pressure & geometric distributions at selected spanstation comparing  11 datasets calculated for a transporttype wing at several Mach and  AOA combinations




PURPOSE

  • Visualization & Analysis & Comparison of calculated and experimental data.
INPUT
  • Simple & Uniform data input format of multiple data sets
  • Datasets are composed of multiple datasheets.
  • Datasheet have  a columnwise tabular format
  • The structure of a sheet can be line, patch,block, random, line segment, triangular, quadrilateral ..
OUTPUT
  • Screen
  • Postscript files
  • ppm files

OPERATION
  • GUI based on GLUI, GLUT and OpenGL
  • Can also be executed in batch.
SPECIALS (Pre and Postprocessing)
  • Warping of datasets  by efficient volume spline class methods (FSI data or Digital Pressure Painting).    
  • Mollifying of datasets to seed scarse trusted data  in  an other baseline dataset. The results is cardinal with respect to the trusted data  and adheres to the trends of the baseline dataset.
  • Cutting planes (geometric slicer)
  • H continuation of harmonic data
  • Surface Gridding
    • Multiple patches
    • Patch creation/redistribution & assembling
  • Volume Gridding
    • Multiple blocks
    • Hexaeder, tetraeder & prismatic meshes
    • Hyperbolic, elliptic & algebraic generation
    • Elliptic smoothing
    • Analysis
    • Chimera tagging

  • Flutter and Time Trace Analysis
  • PK,PH,K & HK,HH Flutter Analysis
  • Spectral Analysis of Time Traces
  • MIMO identification
GRAPHICS

  • 2d vector drawing mode
    • Multiple figures with  multiple datasets
    • 2 D line and symbol (xy) plots
    • 2 D Vector  (xy-uv) plots
    • 2 D contour (xy-c)  plots
    • 2 D shading (xy-#) plots
    • 3 D line and symbol (xyz) projection plots
    • 3 D Vector  (xyz-uvw) projection plots
    • 3 D contour (xyz-c)  projection plots
    • 3 D shading (xy-#) projection plot

    • Quasi 3D figures with  multiple dataheets
    • Flat layout  figures with multiple datasheets.
  • OpenGL visualization mode
    • Multiple datasets (multiple sheets)
    • 3D geometry (xyz) (patches,  grids)
    • 3D Vectors/Displacements    (uvw)
    • 3D Scalars (c)
    • Contour Lines and  Shading & Scatter
    • Symmetric/anti-symmetric extentions, with respect to ground & wall
    • Blanking
    • Et cetera
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OpenGL  visualization mode demo
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OpenGL  visualization mode demo

Surface pressure, velocity  & geometric distributions  comparing  11 datasets calculated for a transporttype wing at several Mach and  AOA combinations

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Volume pressure, velocity  & geometric distributions  comparing  11 datasets calculated for a transporttype wing at several Mach and  AOA combinations

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Planar Cutting demo
  The volume data (left)  is intersected with 6  cuts (right) which are connected with triangulars


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The first cut  connected with triangulars

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The first cut as scattered data









Mollifying

There are many occasions in which characteristic data describing A/C  systems are scarce/coarse (reduced in order) due to economic reasons (wind tunnel testing, flight testing and Hi-Fi CFD simulations). Examples are tabular data for engines, lift & drag aerodynamic forces, high-fidelity generalised forces needed in flutter certification, Hi-Fi CFD data in optimization processes.  Often a correction method or surrogate model is developed  to continue/interpolate the data.


The mollifyer can be regarded as  injecting the valuable (accurate) scarse data in an already existing dataset in a black box manner. The approach is suitable for impact assessment of design changes, starting data for optimization and  reverse engineering.

Mollifyer demo

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The upper left data is injected in the baseline data (lower left) resulting in the upper right data.  Note that the injected data is invariant  for the mollifying.

Mollifyer demo

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The result is cardinal with respect to the trusted data  and adheres to the trends of the baseline dataset.




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The injected scattered data is visualized after triangularization

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Contours of the baseline and the mollifyed data



Warping Demo
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  The scattered FEM data (left)  is warped  to the  aerodynamic surface (right). The scattered data is also presented at the right.




Warping Demo

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The scattered FEM data (left)  is triangularized. The scattered triangularized data is also presented at the right.





GRID GENERATION 


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A single block grid generated about 5
components.

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A single block grid generated about 9
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A single block grid generated about transportype AC
Flutter and Time Trace Analysis

                                               
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Flutter Analysis, 4 modes

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4 mode extracted MIMO(t) system of generalized airforces compared to the time traces of a simulation.
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Generalized airforces derived from MIMO(t) system
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