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person:("Tanno, Hideyuki")

    LARGE-EDDY SIMULATION OF ROTATING DETONATION WITH A NON-PREMIXED CH4/O2 INJECTION

    Matsuyama, Shingo / Iwata, Kazuya / Nunome, Yoshio et al. | TIBKAT | 2020

    Study on Aerodynamic Characteristics of a High Enthalpy Flow around Blunt-nosed Body

    Takahashi, Masahiro / Satou, Kazuo / Itoh, Katsuhiro et al. | AIAA | 2012

    Flow Visualization inside a Rotating Detonation Engine near Injection Nozzles Using Point-Diffraction Interferometry

    Mizukaki, Toshiharu / Iwasaki, Fumihiko / Kojima, Makoto et al. | AIAA | 2021

      FLOW VISUALIZATION INSIDE A ROTATING DETONATION ENGINE NEAR INJECTION NOZZLES USING POINT-DIFFRACTION INTERFEROMETRY

      Mizukaki, Toshiharu / Iwasaki, Fumihiko / Kojima, Makoto et al. | TIBKAT | 2021

      FLOW VISUALIZATION INSIDE A ROTATING DETONATION ENGINE NEAR INJECTION NOZZLES USING POINT-DIFFRACTION INTERFEROMETRY

      Mizukaki, Toshiharu / Iwasaki, Fumihiko / Kojima, Makoto et al. | TIBKAT | 2021

    Heat flux measurement of Apollo capsule model in the free-piston shock tunnel HIEST

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2009

    Heat Flux Measurement of Apollo Capsule Model at High Stagnation Pressure in Shock Tunnel HIEST

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2018

    Comparison of Re-Entry Flow Computations with High Enthalpy Shock Tunnel Experiments

    Kodera, Masatoshi / Tanno, Hideyuki / Takahashi, Masahiro et al. | AIAA | 2009

    High-Enthalpy Effects on Hypersonic Boundary-Layer Transition

    Wartemann, Viola / Wagner, Alexander / Wagnild, Ross et al. | AIAA | 2018

    Experimental Investigations of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

    Radespiel, Rolf / Ali, Syed R. / Bowersox, Rodney D. et al. | AIAA | 2018

    Free-flight force measurement technique in shock tunnel

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2012

    Aerodynamic Characteristics of Lifting Body HYFLEX under High-Temperature Real-Gas Conditio

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2017

    Effect of Combustor Shape on Scramjet Characteristics at Hypervelocity Condition over Mach 10 Flight

    Takahashi, Masahiro / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2006

    Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

    Takahashi, Masahiro / Sunami, Tetsuji / Tanno, Hideyuki et al. | AIAA | 2005

    Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-off Distance

    Itoh, Katsuhiro / Komuro, Tomoyuki / Tanno, Hideyuki et al. | AIAA | 2009

    HEAT FLUX MEASUREMENT OF APOLLO CAPSULE MODEL AT HIGH STAGNATION PRESSURE IN SHOCK TUNNEL HIEST (AIAA 2018-5264)

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | British Library Conference Proceedings | 2018

    Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

    Takahashi, Masahiro / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2008

    Experimental study on flow establishment in a large scale scramjet

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2001

    Aerodynamic Characteristics of Lifting Body HYFLEX under High-Temperature Real-Gas Conditio (AIAA 2017-0772)

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | British Library Conference Proceedings | 2017