All Stories

  1. Experimental investigation of the shock-induced flow over a wall-mounted cylinder

    Article • Journal of Fluid Mechanics, June 2018, Cambridge University Press

    Hiroshi Ozawa

  2. A highly temperature sensitive and ultra-fast response TSP (Temperature-Sensitive-Paints) for unsteady aerothermodynamics on shock-tube wall

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

    Hiroshi Ozawa

  3. Visualization of Unsteady Boundary-Layer Transition on Shock-Tube Wall using Highly Sensitive Fast-response TSP

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Hiroshi Ozawa

  4. Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited)

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Stuart Laurence, Hiroshi Ozawa