CFD-based aircraft drag prediction and reduction

CFD-based aircraft drag prediction and reduction
February 3-7, 2003; H. Deconinck, K. Sermeus, C. Van Dam

• VAN DAM, C.P. – University of California, Davis, USA
  Aircraft design and the importance of drag prediction
  Critical factors in CFD-based drag prediction
• LESCHZINER, M.A. – Imperial College London, United Kingdom
  Turbulence modeling for aeronautical flows
• VAN DAM, C.P. – University of California, Davis, USA
  Boundary layer transition and its prediction
• TOGNACCINI, R. – Università di Napoli Federico II, Italy
  Methods for drag decomposition, thrust-drag bookkeeping from CFD calculations
• DESTARAC, D. – ONERA, France
  Far-field / near-field drag balance and applications of drag extraction in CFD
• KUSUNOSE, K. – The Boeing Company, USA
  Advanced wake integration method for experimental drag prediction
• LABAN, M. – NLR, The Netherlands
  Application of CFD for drag analysis and validation with wind tunnel data
• MAVRIPLIS, D.J. – National Institute for Aerospace, USA
  Aerodynamic drag prediction using unstructured mesh solvers
• SERMEUS, K. & DECONINCK, H. – von Karman Institute, Belgium
  Drag prediction validation of a multi-dimensional upwind solver
• JAMESON, A. – Stanford University, USA
  Aerodynamic shape optimization using the adjoint method
• WILD, J. & HERRMANN, U. – DLR, Germany
  Designing high-lift systems for low drag