Session Details

OS.2-4:直交格子・適合細分化格子法

Tue. Dec 16, 2025 4:40 PM - 6:20 PM JST
Tue. Dec 16, 2025 7:40 AM - 9:20 AM UTC
Room B: International Conference Room(2nd Floor)
Chair:Daisuke Sasaki

[OS2-4-4-01]2D Aerodynamic Topology Optimization of an Airfoil’s Trailing-Edge Region Using Modified Cellular Automata with Volume of Solid (CAVoS)

*Punnathone Songjakkaew1, Yoshiharu Tamaki3, Taro Imamura2 (1. Graduate Student, Department of Aeronautics and Astronautics, The University of Tokyo, 2. Professor, Department of Aeronautics and Astronautics, The University of Tokyo, 3. Assistant Professor, Department of Aeronautics and Astronautics, The University of Tokyo)

[OS2-4-4-02]Simulation of Flow around a Body on Coarse Grids with Immersed Boundary Method using POD-Galerkin Projection

*Shunta Takahashi1, Takayuki Nagata1, Taku Nonomura1 (1. Nagoya Univ.)

[OS2-4-4-03]This paper reports the results of verifying the impact of geometric shape reproducibility in near-field data on far-field noise preditcion when using Immersed Boundary Method and the FW-H method for evaluating far-field noise.

*Takashi Ishida1, Yoimi Kojima1, Yasushi Ito1, Mitsuhiro Murayama1, Tohru Hirai2, Kentaro Tanaka2 (1. Japan Aerospace Exploration Agency, 2. Ryoyu Systems Co., Ltd.)

[OS2-4-4-04]Integration and Visualization of Surface Physical Quantities in the Immersed Boundary Method

*Ryoji Takaki1 (1. Japan Aeroscape Exploration Agency)

[OS2-4-4-05]Flux-integration-based unsteady aerodynamic force evaluation methods considering conservation errors on non-body-conforming Cartesian grids

*Yuta Omori1, Shigetaka Kawai1, Soshi Kawai1 (1. Tohoku Univ.)