1–20 of 30 hits
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    HAYABUSA2 EARTH RETURN AND SAMPLE RETURN CAPSULE REENTRY

    Saiki, Takanao / Takei, Yuto / Mimasu, Yuya et al. | TIBKAT | 2022

    Prediction of Jet Interaction Heating on a Reentry Capsule (AIAA 2018-0382)

    Miki, Hajime / Fujii, Keisuke | British Library Conference Proceedings | 2018

    Prediction of Jet Interaction Heating on a Reentry Capsule

    Miki, Hajime / Fujii, Keisuke | AIAA | 2018

    Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement

    Numata, Daiju / Fujii, Shota / Nagai, Hiroki et al. | AIAA | 2017

      Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement

      Numata, Daiju | Online Contents | 2017
      Contributors: Fujii, Shota , Asai, Keisuke

      Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement

      Numata, Daiju | Online Contents | 2017
      Contributors: Fujii, Shota , Asai, Keisuke

      Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement

      Numata, Daiju | Online Contents | 2017
      Contributors: Fujii, Shota , Asai, Keisuke

    Pressure Gradient Effects on Supersonic Transition over Axisymmetric Bodies at Incidence

    Tokugawa, Naoko / Choudhari, Meelan / Ishikawa, Hiroaki et al. | AIAA | 2015

      Pressure Gradient Effects on Supersonic Transition over Axisymmetric Bodies at Incidence

      Tokugawa, Naoko | Online Contents | 2015
      Contributors: Fujii, Keisuke

    Development of Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints

    Fujii, Shota / Numata, Daiju / Nagai, Hiroki et al. | AIAA | 2013

    Oscillation of Bow-shock Waves at Hypersonic Speeds

    Fujii, Keisuke / Tsuda, Shoichi / Koyama, Tadao et al. | AIAA | 2013

    CFD Investigation For Obtaining Arcjet Freestream With Higher Dynamic Pressures Using An Arcjet Facility

    Sakai, Takeharu / Fujita, Kazuhisa / Fujii, Keisuke et al. | AIAA | 2013

    Translational temperature distribution measurements in high enthalpy flows by Laser-Induced Fluorescence

    Takayanagi, Hiroki / Shun, Kato / Sakai, Takeharu et al. | AIAA | 2013

    Transition Within Leeward Plane of Axisymmetric Bodies at Incidence in Supersonic Flow

    Tokugawa, N. / Choudhari, Meelan / Ishikawa, Hiroaki et al. | AIAA | 2012

    Conceptual Study on Heat Resistant and Cooling System of Hypersonic Airplanes

    Kojima, Takayuki / Taguchi, Hideyuki / Imamura, Shunsuke et al. | AIAA | 2011

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

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

    Comprehensive Characterization of Test Flows in 110-kW Inductively-Coupled-Plasma Heater

    Fujita, Kazuhisa / Suzuki, Toshiyuki / Mizuno, Masahito et al. | AIAA | 2008

    PIV Measurement of a High-Lift-Device Model in JAXA 6.5m × 5.5m Low-Speed Wind Tunnel

    Kato, Hiroyuki / Watanabe, Shigeya / Hashimoto, Takuro et al. | AIAA | 2007

    PSP Measurement of a High-Lift-Device Model in JAXA 6.5m×5.5m Low-Speed Wind Tunnel

    Mitsuo, Kazunori / Kurita, Mitsuru / Kuchi-Ishi, Shigeru et al. | AIAA | 2007

    Development of Bi-Luminophore Pressure-Sensitive Paint Systems

    Mitsuo, Kazunori / Kurita, Mitsuru / Nakakita, Kazuyuki et al. | IEEE | 2007