Ohwada Taku

Affiliation and department：

Research field (2)： Fluid engineering , Aerospace engineering

Research theme for competitive and other funds (15)：

2019 - 2022 Active TPS for a blunt body behind a strong shock wave by means of subsonic counter-flow jets
2014 - 2017 Theoretical and numerical studies on compressible turbulent flows with shock waves
2009 - 2011 Theory and application of asymptotic numerical method for the incompressible viscous flows
2005 - 2006 New approach in computational fluid dynamics on the basis of kinetic theory
2002 - 2004 MATHEMATICAL AND PHYSICAL STUDIES ON SINGULAR FLUID-DYNAMIC LIMITS FOR THE BOLTZMANN EQUATION

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Papers (41)：

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MISC (5)：

Lectures and oral presentations (9)：

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)
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)
Essence of Shock Capturing
(International Conference on Flow Physics and Its Application, Mathematical research center, National University of Taiwan)
Essence of Shock Capturing
(11th Asian Computational Fluid Dynamics Conference, Dalian University of Technology)
衝撃波捕獲の本質
(京都大学数理解析研究所研究集会「非線形波動現象の数理に関する最近の進展」)

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