大和田 拓

ILES of an array of three subsonic counter-flow jets issuing from a wing leading edge exposed to hypersonic aerodynamic heating 

Advances in Aerodynamics 2(1) 2020年12月  査読有り

Numerical investigation of an active TPS for a wing leading edge exposed to high temperature air behind a strong bow shock wave 

Advances in Aerodynamics 1(1) 2019年12月  査読有り

A simple, robust and efficient high-order accurate shock-capturing scheme for compressible flows: Towards minimalism 

Journal of Computational Physics 362 131 - 162 2018年6月1日  査読有り

On the remedy against shock anomalies in kinetic schemes 

Journal of Computational Physics 255 106 - 129 2013年12月5日  査読有り

Link-wise artificial compressibility method 

JOURNAL OF COMPUTATIONAL PHYSICS 231(15) 5109 - 5143 2012年6月  査読有り

高度に希薄な気体中の加熱物体に働く力 

日本航空宇宙学会誌 34(390) 386 - 395 1986年  招待有り

Three-dimensional numerical simulation of;an;array of;subsonic counter;flow jets issuing;from a wing;leading edge;exposed to hypersonic aerodynamic heating 

French-Japanese Workshop on Wavelet and Large Eddy Representations to Study Turbulent Flows, RIMS, Kyoto University 2019年12月5日   招待有り

Feasibility study of efficient film cooling of wing leading edge exposed to a high temperature gas behind a strong bow shock wave 

1st International Symposium on Advances in Aerodynamics,Chengdu, China   招待有り

Essence of Shock Capturing 

International Conference on Flow Physics and Its Application, Mathematical research center, National University of Taiwan   招待有り

Essence of Shock Capturing 

11th Asian Computational Fluid Dynamics Conference, Dalian University of Technology   招待有り