1–8 von 8 Ergebnissen
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    Experimental and computational investigation of supersonic cavity flows

    Zhang, J. / Morishita, E. / Okunuki, T. et al. | AIAA | 2001

      Experimental and Computational Investigation of Supersonic Cavity Flows

      Zhang, J. / Morishita, E. / Okunuki, T. et al. | British Library Conference Proceedings | 2001

    Spreadsheet Fluid Dynamics for Aeronautical Course Problems

    Morishita, E. / Iwata, Y. / Yuki, K. et al. | British Library Conference Proceedings | 2000

    Study of Continuously Variable Mach Number Flow for a Supersonic Wind Tunnel by the Control of Mass Flow Rate

    Aihara, Y. / Mandai, T. / Morishita, E. et al. | British Library Conference Proceedings | 1994

    ICAS-92-4.9.3 Experimental Investigation of Aerothermal Problems Associated with Hypersonic Flight of HST

    Hozumi, K. / Nomura, S. / Aihara, Y. et al. | British Library Conference Proceedings | 1992

    High-Speed Train in a Reduced Pressure Environment

    Ogawa, A. / Morishita, E. / Japan Society for Aeronautical and Space Services et al. | British Library Conference Proceedings | 1997

    An Inverse Method for the Design of Airfoils

    Nagaoka, T. / Morishita, E. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996

    Unsteady Blade Aerodynamics of a Vertical-axis Wind Turbine

    Makino, D. / Morishita, E. / Japan Society for Aeronautical and Space Services et al. | British Library Conference Proceedings | 1997