1–20 von 26 Ergebnissen
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    Hypersonic aerodynamic research of HOPE using high enthalpy shock tunnel

    Itoh, K. / Komuro, T. / Sato, K. et al. | AIAA | 2001

    Study on surface catalytic effect using high enthalpy shock tunnel

    Ueda, S. / Sato, K. / Komuro, T. et al. | AIAA | 2001

    Ground and Flight Testing of Scramjet in NAL-KSPL

    Tanno, H. / Itoh, K. / Ueda, S. et al. | British Library Conference Proceedings | 2002

    Effect of Wall Catalycity on Aerodynamic Heating of Flat Plates in a High Enthalpy Shock Tunnel

    Ueda, S. / Sato, K. / Komuro, T. et al. | British Library Conference Proceedings | 2002

    6-3 Improvements of Accelerometer Force Measurement Technique

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2005

    5-2 Experimental Investigations of the Flow Field around a Generic Re-entry Capsule in HIEST

    Hashimoto, T. / Itoh, K. / Komuro, T. et al. | British Library Conference Proceedings | 2005

    Scramjet Characteristics at Hypervelocity Condition over Mach 10 Flight - Application of a Diverging Combustor

    Takahashi, M. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2006

    Performance Characteristics of Scramjet Engine with Different Combustor Shapes at Hypervelocity Condition over Mach 10 Flight AIAA Paper

    Takahashi, M. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2007

    Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST

    Tanno, H. / Sato, K. / Komuro, T. et al. | British Library Conference Proceedings | 2008

    Aerodynamic Characteristics of Generic Models Under Real-Gas Condition in the Free-Piston Shock Tunnel HIEST

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2008

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

    Takahashi, M. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2008

    Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2009

    Influence of Thermal Non-Equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST

    Takahashi, M. / Kodera, M. / Itoh, K. et al. | British Library Conference Proceedings | 2009

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

    Itoh, K. / Komuro, T. / Tanno, H. et al. | British Library Conference Proceedings | 2009

    Heat Flux Measurement of Apollo Capsule Model in the Free-Piston Shock Tunnel HIEST

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2009

    AEROHEATING MEASUREMENT OF A RE-ENTRY CAPSULE MODEL IN FREE-PISTON SHOCK TUNNEL HIEST

    Tanno, H. / Kodera, M. / Komuro, T. et al. | British Library Conference Proceedings | 2010

    MEASUREMENT OF HYPERSONIC HIGH-ENTHALPY BOUNDARY LAYER TRANSITION ON 7^o CONE MODEL

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2010

    MEASUREMENT OF SURFACE PRESSURE FLUCTUATION IN HYPERSONIC HIGH-ENTHALPY BOUNDARY LAYER ON A 7-DEGREE CONE MODEL

    Tanno, H. / Komuro, T. / Sato, K. et al. | British Library Conference Proceedings | 2011