STS272A Towards Next-Generation Aircraft Design with High-Fidelity Simulation Technologies I
MS Corresponding Organizer: Dr. Yoshiaki Abe ( Tohoku University , Japan )
Chaired by:
Dr. Yoshiaki Abe ( Tohoku University , Japan ) , Prof. Shigeru Obayashi ( Tohoku University , Japan )
Dr. Yoshiaki Abe ( Tohoku University , Japan ) , Prof. Shigeru Obayashi ( Tohoku University , Japan )
Scheduled presentations:
-
Influences of Multiple Winglets on the Aerodynamic Performance and Flow Field of a Civil Aircraft
E. Kobayashi*, K. Chiba, M. Kanazaki -
Identification of losses from engine-airframe interaction for a passenger aircraft through integrated simulation
J. Mueller*, K. Chiba, Y. Oba -
Upper Surface Morphing for Drag Minimization in NACA 641−612 Airfoil
G. Vigneswar*, S. Faruque Ali, A. Arunachalakasi -
Multi-objective design of CFRP composite aircraft wing with next generation fibers and resins
Y. Liu*, T. Yamazaki, S. Date, T. Nagashima, Y. Abe -
Structural cohesive element for the modelling of delamination between thin shells without cohesive zone limit
X. Ai, B. Chen*, C. Kassapoglou -
Laminarization of Supersonic Three-dimensional Boundary Layer by Sinusoidal Roughness Elements
M. Hirota*, S. Niwano, Y. Ide, Y. Hattori, S. Obayashi -
On the Extension of the CFD Solver CODA for Turbomachinery Applications
G. Ashcroft*, A. Bleh, H. Birliker, P. Post
