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Kashitani Masashi  樫谷 賢士

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KASHITANI Masashi  樫谷 賢士

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Researcher Number 80535279
Affiliation (Current) 2026: 防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群), システム工学群, 教授
Affiliation (based on the past Project Information) *help 2021 – 2024: 防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群), システム工学群, 教授
2017 – 2019: 防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群), システム工学群, 教授
2014 – 2016: 防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工, システム工学群, 教授
2009 – 2010: 防衛大学校, システム工学群, 准教授
Review Section/Research Field
Principal Investigator
Basic Section 24010:Aerospace engineering-related / Aerospace engineering / Fluid engineering
Keywords
Principal Investigator
空力特性 / 可視化 / 風洞試験 / 超音速複葉翼 / 三次元流れ / シュリーレン法 / 抵抗低減 / ブーゼマン複葉翼 / 衝撃波管 / 超音速風洞 … More / ソニックブーム / 風洞技術 / 遷音速流れ / 空力測定技術 / ライトフィールド光学 / ライトフィールド光学系 / シュリーレン / 遷音速 / 低レイノルズ数流れ / 空気力学 / 低レノルズ数 / 高分解能 / 数値シミュレーション / 翼型 / 翼型流れ / 高揚力装置 / 低レイノルズ数 / 点回折干渉計 / 抵抗 / 低温風洞 / 後流 / 高レイノルズ数流れ / 数値計算 / 圧縮性流体 / 圧縮性流れ / 流体計測 Less
  • Research Projects

    (5 results)
  • Research Products

    (60 results)
  •  超音速噴流を利用した高速風洞によるブーゼマン複葉翼機の実現にむけた抵抗特性の解明Principal Investigator

    • Principal Investigator
      樫谷 賢士
    • Project Period (FY)
      2024 – 2026
    • Research Category
      Grant-in-Aid for Scientific Research (C)
    • Review Section
      Basic Section 24010:Aerospace engineering-related
    • Research Institution
      防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群)
  •  Measurement of Flow Fields and Aerodynamics of Transonic Three-Dimensional Biplane Using Light Field OpticsPrincipal Investigator

    • Principal Investigator
      Kashitani Masashi
    • Project Period (FY)
      2021 – 2023
    • Research Category
      Grant-in-Aid for Scientific Research (C)
    • Review Section
      Basic Section 24010:Aerospace engineering-related
    • Research Institution
      防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群)
  •  Development of a Double Path PDI Method of Two-Wavelength Light Source and Investigation of the Airfoil Characteristics in a Low-Reynolds Number High-Subsonic FlowPrincipal Investigator

    • Principal Investigator
      Kashitani Masashi
    • Project Period (FY)
      2017 – 2019
    • Research Category
      Grant-in-Aid for Scientific Research (C)
    • Research Field
      Aerospace engineering
    • Research Institution
      防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群)
  •  Study on establishment of cryogenic wind tunnel testing for flow visualizations in a high Reynolds number flowPrincipal Investigator

    • Principal Investigator
      Kashitani Masashi
    • Project Period (FY)
      2014 – 2016
    • Research Category
      Grant-in-Aid for Scientific Research (C)
    • Research Field
      Aerospace engineering
    • Research Institution
      防衛大学校(総合教育学群、人文社会科学群、応用科学群、電気情報学群及びシステム工学群)
  •  Study of application and density measurements by focusing schlieren method in high speed flowsPrincipal Investigator

    • Principal Investigator
      KASHITANI Masashi
    • Project Period (FY)
      2009 – 2010
    • Research Category
      Grant-in-Aid for Young Scientists (B)
    • Research Field
      Fluid engineering
    • Research Institution
      防衛大学校

All 2025 2024 2023 2022 2021 2020 2019 2018 2017 2016 2015 2014 2011 2010 2009 Other

All Journal Article Presentation Book

  • [Book] 空気力学の基礎(J. D. Anderson, Jr., Fundamentals of Aerodynamics, 翻訳)2016

    • Author(s)
      山口裕,樫谷賢士
    • Total Pages
      1088
    • Publisher
      プレアデス出版
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Journal Article] Analysis of stagger effects on Busemann supersonic biplane airfoil in shock tube tests by point diffraction interferometer method2022

    • Author(s)
      T. D. Nguyen, M. Taguchi, K. Tsuji, M. Kashitani, H. Tanno, K. Kusunose
    • Journal Title

      Aerospace Science and Technology

      Volume: 131 Pages: 1-14

    • DOI

      10.1016/j.ast.2022.107957

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Journal Article] Effects of Stagger on Low-speed Performance of Busemann Biplane Airfoil2022

    • Author(s)
      T. D. Nguyen, M. Kashitani, M. Taguchi, K. Kusunose
    • Journal Title

      Aerospace

      Volume: 9 Issue: 4 Pages: 1-23

    • DOI

      10.3390/aerospace9040197

    • Peer Reviewed / Open Access
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Journal Article] Analysis of a Wing-Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow2022

    • Author(s)
      Thai Duong Nguyen , Masashi Kashitani, Kazuhiro Kusunose, Masato Taguchi, Yoshihiro Takita
    • Journal Title

      Journal of Aircraft

      Volume: 59 Issue: 2 Pages: 350-365

    • DOI

      10.2514/1.c036154

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Journal Article] Fundamental Study on PIV Analysis of Flow Field Visualized by Focusing Schlieren Method2021

    • Author(s)
      樫谷賢士,田口正人
    • Journal Title

      AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

      Volume: 20 Issue: 0 Pages: 97-100

    • DOI

      10.2322/astj.20.97

    • NAID

      130008074228

    • ISSN
      1884-0477
    • Language
      Japanese
    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Journal Article] Fundamental Study on Operational Conditions of Diaphragmless Shock Tube Driven by Pneumatic Piston2018

    • Author(s)
      Masato Taguchi, Masashi Kashitani and Masanori Nishiyama
    • Journal Title

      International Journal of Mechanical Engineering and Robotics Research

      Volume: 7 Pages: 649-655

    • DOI

      10.18178/ijmerr.7.6.649-655

    • Peer Reviewed / Open Access
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Journal Article] A Study on High Subsonic Airfoil Flows in Relatively High Reynolds Number by OpenFOAM2014

    • Author(s)
      Shinichiro NAKAO, Masashi KASHITANI, Takeshi MIYAGUNI, Yutaka YAMAGUCHI
    • Journal Title

      Journal of Thermal Science

      Volume: 23 Pages: 133-137

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Journal Article] Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method2011

    • Author(s)
      M.Kashitani, Y.Yamaguchi, H.Kitano
    • Journal Title

      AIAA Paper

      Pages: 2011-983

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Journal Article] 点回折干渉計による衝撃波管翼型流れの試験気体の影響に関する研究2011

    • Author(s)
      樫谷賢士, 山口裕, 沖元海
    • Journal Title

      日本航空宇宙学会論文集

      Volume: 59 Pages: 34-41

    • NAID

      10028049093

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Journal Article] 点回折干渉計による衝撃波管翼型流れの試験気体の影響に関する研究2011

    • Author(s)
      樫谷賢士, 山口裕, 沖元海
    • Journal Title

      日本航空宇宙学会論文集 59

      Pages: 34-41

    • NAID

      10028049093

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Journal Article] フォーカシングシュリーレン画像による密度計測に関する基礎実験2010

    • Author(s)
      樫谷賢士, 山口裕, 北野秀樹
    • Journal Title

      可視化情報学会誌 Vol.30, Suppl.No.2

      Pages: 115-116

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Journal Article] Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Testing2010

    • Author(s)
      M.Kashitani
    • Journal Title

      Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows No.4C-3

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Journal Article] Visualizations around the 3-D Diamond Model with Trip Strips in Transonic Shock Tube Flows by Focusing Schlieren Method2010

    • Author(s)
      M.Kashitani, Y.Yamaguchi, G.Oki
    • Journal Title

      Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows No.5C-1

    • Peer Reviewed
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] 遷音速および高亜音速における超音速複葉翼機の空力特性に関する基礎研究2025

    • Author(s)
      樫谷賢士,田口正人,兵藤佑都
    • Organizer
      2024年度衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-24K07898
  • [Presentation] 点回折干渉計法によるフラップを有するBusemann複葉翼まわりの遷音速流れの可視化2024

    • Author(s)
      樫谷賢士, 田口正人,辻康平
    • Organizer
      2023年度衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] Wake Measurement on a Three-Dimensional Model of Staggered Busemann Biplane in NDA 1.5m Low Speed Wind Tunnel2023

    • Author(s)
      Masato TAGUCHI and Masashi KASHITANI
    • Organizer
      Subsonic Aerodynamic Testing Association 57th Meeting
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] 遷音速流れのブーゼマン複葉翼間に発生する衝撃波について2023

    • Author(s)
      田口正人,グエンタイズオン,辻康平,樫谷賢士
    • Organizer
      2022年度衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] Visualization of Transonic Flow around Flapped Busemann Biplane Airfoil by Point Diffraction Interferomenter2023

    • Author(s)
      Masato TAGUCHI, Masashi KASHITANI and Kohei TSUJI
    • Organizer
      20th International Symposium on Flow Visualization
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] 風洞実験に向けたライトフィールドカメラを用いた流れ場の可視化に関する基礎研究2022

    • Author(s)
      辻康平,田口正人,樫谷賢士,仲尾晋一郎,宮里義昭
    • Organizer
      流体力学講演会
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] ライトフィールド光学系による流れ場の可視化に関する基礎研究2022

    • Author(s)
      辻康平,田口正人,樫谷賢士, 仲尾晋一郎,宮里義昭
    • Organizer
      2021衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] Preliminary Study for Flow Field Diagnostics Using a Light Field Camera2022

    • Author(s)
      M. Kashitani, M. Taguchi, K. Tuji, S. Nakao, Y. Miyazato
    • Organizer
      9th AJWTFS 2022
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] Aerodynamic Characteristics of Busemann Biplane Installed with High-Lift Device Using Low-Speed Smoke Wind Tunnel2022

    • Author(s)
      Masashi Kashitani, Nguyen T. Duong, Masato Taguchi, Kazuhiro Kusunose
    • Organizer
      AIAA Paper 2022-0140
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] An Experimental Investigation of Busemann Biplane in Transonic Flow by Focusing Schlieren Technique2022

    • Author(s)
      Thai Duong Nguyen, Masato Taguchi, Masashi Kashitani
    • Organizer
      AIAA Paper 2022 0769
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] PDI法によるブーゼマン複葉翼の翼間流れに関する研究2022

    • Author(s)
      グエン タイ ズオン,辻康平,田口正人,樫谷賢,楠瀬一洋
    • Organizer
      2021衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] Analysis of Low-speed Aerodynamic Characteristics of Busemann Biplane Airfoil installed High Lift Devices2022

    • Author(s)
      , T. D. Nguyen, M. Kashitani, M. Taguchi, K. Kusunose
    • Organizer
      33rd ICAS 2022
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] ブーゼマン複葉翼の遷音速衝撃波管流れ場に関する光学計測2022

    • Author(s)
      樫谷賢士,田口正人,辻康平,グエンタイズオン,楠瀬一洋
    • Organizer
      第60回飛行機シンポジウム
    • Data Source
      KAKENHI-PROJECT-21K04495
  • [Presentation] A Preliminary Study of Shock Tube SC Airfoil Flows with Gurney Flap by utilizing PDI2020

    • Author(s)
      M. Kashitani, M. Taguchi N. Thai Duong, A. Oomori, M. Nishiyama, H. Tanno
    • Organizer
      AIAA Scitech 2020 Forum
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 点回折干渉計を用いた小型高揚力装置を伴う遷速翼型流れの可視化2019

    • Author(s)
      田口正人,西山真悟,大森朗徳,樫谷賢士,丹野英幸
    • Organizer
      第57回飛行機シンポジウム
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 紫外光線を用いた点回折干渉計による遷音速衝撃波管翼型流れの可視化に関する基礎研究2019

    • Author(s)
      大森朗徳,田口正人,樫谷賢士,丹野英幸
    • Organizer
      第63回宇宙科学技術連合講演会
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 空間分解能を向上した点回折干渉計による衝撃波管翼型流れ の可視化実験2018

    • Author(s)
      西山 真悟, 樫谷 賢士, 田口正人
    • Organizer
      第62回宇宙科学技術連合講演会
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 点回折干渉計による低レイノルズ数流れの可視化に向けた基礎研究2018

    • Author(s)
      西山真悟,田口正人,樫谷賢士,宮崎大
    • Organizer
      平成29年度衝撃波シンポジウム
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 点回折干渉計による流れ場解析について の一考2018

    • Author(s)
      樫谷 賢士, 田口正人, 西山 真悟
    • Organizer
      第46回 可視化情報シンポジウム
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 衝撃波管による空力試験について2018

    • Author(s)
      樫谷賢士,田口正人,西山真悟
    • Organizer
      第56回 飛行機シンポジウム
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] Visualization Around Shock Tube Airfoil Flows Utilizing Point Diffraction Interferometer2018

    • Author(s)
      Masashi Kashitani, Masato Taguchi, Dai Miyazaki, Masayoshi Nishiyama
    • Organizer
      18th International Symposium on Flow Visualization
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] Aerodynamic Investigations on SC-0414 Airfoil with Small High Lift Devices2018

    • Author(s)
      Nguyen Thai Duong, Masashi Kashitani and Masato Taguchi
    • Organizer
      2018 Asia Conference on Mechanical and Aerospace Engineering
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] ピストン駆動による無隔膜衝撃波管の作動特性に関する基礎研究2017

    • Author(s)
      西山真悟,田口正人,樫谷賢士
    • Organizer
      可視化情報全国講演会 (室蘭2017)
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] Fundamental Study on Operational Parameters of Diaphragmless Shock Tube2017

    • Author(s)
      Masanori NISHIYAMA, Masato TAGUCHI, Masashi KASHITANI
    • Organizer
      2017 Asia Conference on Mechanical and Aerospace Engineering
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] 衝撃波管を用いた低レイノルズ数翼型流れに関する研究2017

    • Author(s)
      田口正人,樫谷賢士,宮崎大,西山真悟
    • Organizer
      第55回 飛行機シンポジウム
    • Data Source
      KAKENHI-PROJECT-17K06956
  • [Presentation] LED光源を用いたフォーカシングシュリーレン PIV法に関する基礎研究2016

    • Author(s)
      樫谷賢士,滝田好宏,三浦圭太,宮里義昭,仲尾晋一郎
    • Organizer
      第54回飛行機シンポジウム
    • Place of Presentation
      富山県,富山国際会議場/ANAクラウンプラザホテル
    • Year and Date
      2016-10-24
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] Consideration of aerodynamic test model for low speed wind tunnel in NDA2016

    • Author(s)
      Masashi Kashitani, Yoshihiro Takita, Yutaka Yanaguchi
    • Organizer
      52th Annual Subsonic Aerodynamic Testing Association Meeting
    • Place of Presentation
      Lucerne, Switzerland
    • Year and Date
      2016-06-05
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] A Preliminary Study on Calibration Method for a Balance System in a Cryogenic Wind Tunnel2016

    • Author(s)
      Masashi Kashitani, Hiroaki Ono, Yutaka Yamaguchi
    • Organizer
      The 2016 Asia-Pacific International Symposium on Aerospace Technology
    • Place of Presentation
      Toyama, Japan
    • Year and Date
      2016-10-25
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] 簡易な3Dプリンターを用いた航空機の 設計教育に関する一考2016

    • Author(s)
      樫谷賢士,滝田好宏,大川真弥,山口裕
    • Organizer
      第47期日本航空宇宙学会年会講演会
    • Place of Presentation
      東京大学,山上会館
    • Year and Date
      2016-04-14
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] 超音速流れにおける双胴模型の空力特性に関する基礎実験2016

    • Author(s)
      樫谷賢士
    • Organizer
      平成27年度衝撃波シンポジウム
    • Place of Presentation
      熊本大学工学部(熊本県,熊本市)
    • Year and Date
      2016-03-07
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] A Study on Aerodynamic Characteristics of Aircraft Model with Vortex Generators by Wake Measurements2015

    • Author(s)
      Masashi Kashitani
    • Organizer
      2015 Asia-Pacific International Symposium on Aerospace Technology
    • Place of Presentation
      Queensland, Australia
    • Year and Date
      2015-11-25
    • Int'l Joint Research
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] 半裁模型用風洞天秤の校正法に関する予備研究2015

    • Author(s)
      樫谷賢士
    • Organizer
      第53回飛行機シンポジウム
    • Place of Presentation
      松山市総合コミュニティセンター(愛媛県,松山市
    • Year and Date
      2015-11-11
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] 低温風洞で用いる半裁模型用風洞天秤の校正法に関する基礎実験2015

    • Author(s)
      樫谷賢士
    • Organizer
      日本航空宇宙学会西部支部講演会
    • Place of Presentation
      広島大学東広島キャンパス(広島県,東広島市)
    • Year and Date
      2015-12-04
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method2011

    • Author(s)
      M.Kashitani, Y.Yamaguchi, H.Kitano
    • Organizer
      49th AIAA Aerospace Sciences Meeting
    • Place of Presentation
      Orlando World Center Marriott Orlando, Florida
    • Year and Date
      2011-01-05
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] Preliminary Study for Quantitative Measurement of Flow Fields by Focusing Schlieren Method2011

    • Author(s)
      M.Kashitani, Y.Yamaguchi, H.Kitano
    • Organizer
      49th AIAA Aerospace Sciences Meeting
    • Place of Presentation
      Orlando
    • Year and Date
      2011-01-05
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] フォーカシングシュリーレン画像による密度計測に関する基礎実験2010

    • Author(s)
      樫谷賢士, 山口裕, 北野秀樹
    • Organizer
      可視化情報学会全国講演会
    • Place of Presentation
      鹿児島
    • Year and Date
      2010-10-07
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] 衝撃波管を用いた超音速複葉翼型流れに関する基礎研究2010

    • Author(s)
      樫谷賢士, 山口裕, 沖元海, 江刺悟, 楠瀬一洋
    • Organizer
      日本航空宇宙学会第41期年会講演会
    • Place of Presentation
      東京
    • Year and Date
      2010-04-16
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] 高亜音速衝撃波管翼型流れの可視化2010

    • Author(s)
      山口裕, 沖元海, 宮崎大, 樫谷賢士, 江刺悟
    • Organizer
      第48回飛行機シンポジウム
    • Place of Presentation
      静岡コンベンションアーツセンターグランシップ(静岡県 静岡市)
    • Year and Date
      2010-11-30
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] OpenFOAMを用いた3次元模型周りの流れ場の診断2010

    • Author(s)
      江刺悟, 山口裕, 樫谷賢士, 沖元海
    • Organizer
      平成21年度衝撃波シンポジウム
    • Place of Presentation
      埼玉
    • Year and Date
      2010-03-17
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] フォーカシングシュリーレン画像による密度計測に関する基礎実験2010

    • Author(s)
      樫谷賢士, 山口裕, 北野秀樹
    • Organizer
      可視化情報学会全国講演会
    • Place of Presentation
      霧島市国分シビックセンター(鹿児島県 霧島市)
    • Year and Date
      2010-10-07
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] 高亜音速衝撃波管翼型流れの可視化2010

    • Author(s)
      山口裕, 沖元海, 宮崎大, 樫谷賢士, 江刺悟
    • Organizer
      第48回飛行機シンポジウム
    • Place of Presentation
      静岡
    • Year and Date
      2010-12-02
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] Visualizations around the 3-D Diamond Model with Trip Strips in Transonic Shock Tube Flows by Focusing Schlieren Method2009

    • Author(s)
      M.Kashitani
    • Organizer
      9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows
    • Place of Presentation
      Gyeongju TEMF Hotel(Korea)
    • Year and Date
      2009-09-11
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Testing2009

    • Author(s)
      M.Kashitani
    • Organizer
      9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows
    • Place of Presentation
      Gyeongju TEMF Hotel(Korea)
    • Year and Date
      2009-09-11
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] Visualizations around the 3-D Diamond Model with Trip Strips in Transonic Shock Tube Flows by Focusing Schlieren Method2009

    • Author(s)
      M.Kashitani, Y.Yamaguchi, G.Oki
    • Organizer
      9th ISAIF
    • Place of Presentation
      Gyeongju
    • Year and Date
      2009-09-11
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Testing2009

    • Author(s)
      M.Kashitani
    • Organizer
      9th ISAIF
    • Place of Presentation
      Gyeongju
    • Year and Date
      2009-09-11
    • Data Source
      KAKENHI-PROJECT-21760144
  • [Presentation] 小型低温風洞における半裁模型風洞天秤に関する予備実験

    • Author(s)
      樫谷賢士, 山口裕, 谷野忠和, 小野洋彰
    • Organizer
      平成26年度衝撃波シンポジウム
    • Place of Presentation
      群馬県,渋川市
    • Year and Date
      2015-03-09 – 2015-03-11
    • Data Source
      KAKENHI-PROJECT-26420821
  • [Presentation] Experimental Study on Aerodynamic Characteristics of Blended-Wing-Body by a Wake Integration Method

    • Author(s)
      Masashi KASHITANI, Yoshie SUGANUMA, Hisashi DATE, Shinichiro NAKAO,Yoshihiro TAKITA, Yutaka YAMAGUCHI
    • Organizer
      53rd AIAA Aerospace Sciences Meeting
    • Place of Presentation
      Kissimmee , Florida
    • Year and Date
      2015-01-05 – 2015-01-09
    • Data Source
      KAKENHI-PROJECT-26420821

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