Rchr
J-GLOBAL ID:201401004750544391   Update date: Jan. 30, 2024

Ohwada Taku

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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