Scheduled presentations:

• Influences of Multiple Winglets on the Aerodynamic Performance and Flow Field of a Civil Aircraft
  *E. Kobayashi (The University of Electro-Communications), K. Chiba (The University of Electro-Communications), M. Kanazaki (Tokyo Metropolitan University)
• Identification of losses from engine-airframe interaction for a passenger aircraft through integrated simulation
  *J. Mueller (The University of Electro-Communications), K. Chiba (The University of Electro-Communications), Y. Oba (IHI)
• Upper Surface Morphing for Drag Minimization in NACA 641−612 Airfoil
  *G. Vigneswar (INDIAN INSTITUTE OF TECHNOLOGY MADRAS), S. Faruque Ali (INDIAN INSTITUTE OF TECHNOLOGY MADRAS), A. Arunachalakasi (INDIAN INSTITUTE OF TECHNOLOGY MADRAS)
• Multi-objective design of CFRP composite aircraft wing with next generation fibers and resins
  *Y. Liu (Institute of Fluid Science, Tohoku University), T. Yamazaki (Institute of Fluid Science, Tohoku University), S. Date (Institute of Fluid Science, Tohoku University), T. Nagashima (Faculty of Science and Technology, Sophia Un), Y. Abe (Institute of Fluid Science, Tohoku University)
• Structural cohesive element for the modelling of delamination between thin shells without cohesive zone limit
  X. Ai (TU Delft), *B. Chen (TU Delft), C. Kassapoglou (TU Delft)
• Laminarization of Supersonic Three-dimensional Boundary Layer by Sinusoidal Roughness Elements
  *M. Hirota (Tohoku University), S. Niwano (Tohoku University), Y. Ide (Japan Aerospace Exploration Agency), Y. Hattori (Tohoku University), S. Obayashi (Tohoku University)
• On the Extension of the CFD Solver CODA for Turbomachinery Applications
  *G. Ashcroft (German Aerospace Center), A. Bleh (German Aerospace Center), H. Birliker (German Aerospace Center), P. Post (Airbus)