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  • Abstract
  • Definition of the test case
  • Physical and Mathematical modelling
  • Methodology
  • Analysis of the results
  • Results
  • Files
  • Comments

A common platform for validation of aircraft drag reduction technologies

  • Geometry
  • SOLVER_SBW.bmap
  • MESH SBW.zip
  • MESH SBW.z09
  • MESH SBW.z08
  • MESH SBW.z07
  • MESH SBW.z06
  • MESH SBW.z05
  • MESH SBW.z04
  • MESH SBW.z03
  • MESH SBW.z02
  • MESH SBW.z01
  • SOLVER_parameters.txt
  • parameters.txt
  • SBW Re27.3e6 M0.72 a1.0.surface.pval.120000.dat
  • SBW.bmap
  • SBW.igs
  • SBW Re27.3e6 M0.72 a1.0.pval.120000 Shock point format.dat.txt
  • SBW Re27.3e6 M0.72 a1.0.pval.120000 Shock.plt.txt
  • SBW su2.zip.txt
  • SBW.cgns.txt
  • SBW.grid.txt
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Website coordinator: sara.guttilla@euromech.org
The E-CAero2 project (2014-2017) funded within H2020 is the natural follow-up of the E-CAero project (2009-2013) developed within FP7
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