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    Aerodynamic characteristics of generic models under real-gas condition in the free-piston shock tunnel HIEST

    Tanno, Hideyuki / Sato, Kazuo / Komuro, Tomoyuki et al. | AIAA | 2008

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

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

    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

    Aerodynamic Evaluation of a Capsule Shaped Projectile during Free Flight Testing with Ballistic Range

    Ishida, Akiho / Nagai, Hiroki / Tanno, Hideyuki et al. | AIAA | 2015

    Aerodynamic Evaluation of a Capsule Shaped Projectile during Free Flight Testing with Ballistic Range (AIAA 2015-0244)

    Ishida, Akiho / Nagai, Hiroki / Tanno, Hideyuki et al. | British Library Conference Proceedings | 2015

    Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST

    Tanno, Hideyuki / Sato, Kazuo / Komuro, Tomoyuki et al. | AIAA | 2008

    Basic characteristics of the free-piston driven expansion tube JAXA HEK-X

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2016

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

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

    Development of a new force measurement method for scramjet testing in a high enthalpy shock tunnel

    Takahashi, M. / Ueda, Shuichi / Komuro, Tomoyuki et al. | AIAA | 1999

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

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

    Experimental Study of High-Enthalpy Heat Flux Augmentation in Shock Tunnels

    Tanno, Hideyuki / Komuro, Tomoyuki / Lillard, Randolph P. et al. | AIAA | 2015

    Experimental study on flow establishment in a large scale scramjet

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

    Experimental Study on Heat Flux Augmentation in High-enthalpy Shock Tunnels

    Tanno, Hideyuki / Komuro, Tomoyuki / Ohnishi, Naofumi et al. | AIAA | 2014

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

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

    Free-flight aerodynamic test of elliptic cone in Shock Tunnel

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2015

    Free-flight Aerodynamic Test of Elliptic Cone in Shock Tunnel (AIAA 2015-3655)

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | British Library Conference Proceedings | 2015

    Free-flight aerodynamic tests of reentry vehicles in high-temperature real-gas flow (Invited)

    Tanno, Hideyuki / Sato, Kazuo / Komuro, Tomoyuki et al. | AIAA | 2014

    Free-flight aerodynamic test with projectile-onboard data recorder in a ballistic range

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2013

    Free-flight force measurement technique in shock tunnel

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

    Free-flight tests of reentry capsule models in free-piston shock tunnel

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2013

    Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | AIAA | 2017

    Global Heat Flux Measurement Using Temperature-Sensitive Paint in High-Enthalpy Shock Tunnel HIEST (AIAA 2017-1682)

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | British Library Conference Proceedings | 2017

    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

    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

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

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

    High-speed visualization for test-time evaluation of a JAXA HEK-X free-piston driven expansion tube

    Shimamura, Kohei / Okamoto, Atsushi / Fujiwara, Yusuke et al. | AIAA | 2019

    Hypervelocity aerothermodynamic and propulsion research using a high enthalpy shock tunnel HIEST

    Itoh, Katsuhiro / Ueda, Shuichi / Komuro, Tomoyuki et al. | AIAA | 1999

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

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

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

    Takahashi, Masahiro / Kodera, Masatoshi / Itoh, Katsuhiro et al. | AIAA | 2009

    Laser Absorption Spectroscopy for Determination of Flow Characteristics in High Enthalpy Shock Tunnel

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2006

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

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

    Measurement of hypersonic high-enthalpy boundary layer transition on a 7º cone model

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2010

    Measurement of surface pressure fluctuation in hypersonic high-enthalpy boundary layer on a 7-degree cone model

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2011

    Measurement of Ultraviolet Radiative Heating Augmentation in HIEST Reflected Shock Tunnel

    Cruden, Brett A. / Brandis, Aaron M. / Grinstead, Jay H. et al. | AIAA | 2015

    Miniature Data-Logger for Aerodynamic Force Measurement in Impulsive Facility

    Tanno, Hideyuki / Sato, Kazuo / Takahashi, Masahiro et al. | AIAA | 2010

    Numerical Analysis of Experimental Results on the Surface Catalycity in HIEST

    Ueda, Shuichi / Sato, Kazuo / Komuro, Tomoyuki et al. | AIAA | 2005

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

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

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

    Takahashi, Masahiro / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2007

    Porous Injection Effect on Surface Heat Flux in High-enthalpy High-Reynolds number flow

    Tanno, Hideyuki / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2016

    Resonant growth of surface pressure fluctuation in hypersonic boundary layer in shock tunnel

    Itoh, Katsuhiro / Tanno, Hideyuki / Komuro, Tomoyuki | AIAA | 2017

    Spectroscopic Investigation on Anomalous Heating in Free Piston Shock Tunnel HIEST

    Nomura, Satoshi / Takayanagi, Hiroki / Fujita, Kazuhisa et al. | AIAA | 2014

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

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

    Visualization of Hypersonic Boundary Layer Transition on Elliptic Cone in High Enthalpy Shock Tunnel with Temperature-Sensitive Paint

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | AIAA | 2016

    Visualization of Hypersonic Boundary Layer Transition on Elliptic Cone in High Enthalpy Shock Tunnel with Temperature-Sensitive Paint (AIAA 2016-0358)

    Nagayama, Takehiro / Nagai, Hiroki / Tanno, Hideyuki et al. | British Library Conference Proceedings | 2016

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