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    METHODS AND APPARATUS FOR ACCELERATING AN AIRCRAFT FUSELAGE BOUNDARY LAYER VIA A FAN POWERED BY AN AUXILIARY POWER UNIT OF THE AIRCRAFT

    Freier Zugriff
    PRINCEN NORMAN H / LIEBECK ROBERT H / SATO SHO | Europäisches Patentamt | 2022

      Methods and apparatus for accelerating an aircraft fuselage boundary layer via a fan powered by an auxiliary power unit of the aircraft

      Freier Zugriff
      PRINCEN NORMAN H / LIEBECK ROBERT H / SATO SHO | Europäisches Patentamt | 2023

    Flight Evaluation of an LPV Sliding Mode Observer for Sensor FTC

    Freier Zugriff
    Chen, L / Alwi, H / Edwards, C et al. | BASE | 2022

    Development of a next generation ATP system

    Sato, K. / Arai, H. | IEEE | 2001

    Mach number control of Ludwieg tubes

    SATO, J. / TANEDA, H. | AIAA | 1986

    Measurement of Supersonic Flow Field using Particle Tracking Velocimetry

    Nakamura, H. / Sato, N. / Kobayashi, H. et al. | IEEE | 2005

    Performance characteristics of ring-cusp ion thruster

    TAKEGAHARA, H. / SHIMADA, S. / SATO, K. | AIAA | 1987

    Polarization bistable characteristics of mesa structure 980 nm VCSELs

    Sato, Y. / Mori, T. / Yamayoshi, Y. et al. | IEEE | 2005