All Stories

  1. Direct Numerical Simulation of Shock Waves Passed by Multiple Particles by Using Immersed Boundary Method

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Shun Takahashi, Mr. Takayuki Nagata, Taku Nonomura

  2. Analysis of the Temperature Ratio Effects on the Flow Properties of the Low Reynolds and High Mach number Flow around a Sphere

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Shun Takahashi, Mr. Takayuki Nagata, Taku Nonomura