Kanda Takeshi 苅田丈士

Researcher Number	50358545
Affiliation (Current)	2023: 中部大学, 理工学部, 教授 2023: 国立研究開発法人宇宙航空研究開発機構, 研究開発部門, 上席研究開発員
Affiliation (based on the past Project Information) *help	2018 – 2021: 中部大学, 工学部, 教授
Review Section/Research Field	Principal Investigator Basic Section 19010:Fluid engineering-related / Basic Section 19020:Thermal engineering-related
Keywords	Principal Investigator タービン / 超音速 / 遠心力 / 擬似衝撃波 / 性能 / 減速 / 圧縮波 / 亜音速 / 断面積 / 準一次元流れ / ロケットエンジン / 高周波振動 / 燃焼

Research Projects
(2 results)
Research Products
(6 results)

Study of High-Frequency Combustion Instability of Rocket Engines Based on Off-Design Combustion ModelPrincipal Investigator
- Principal Investigator
  
  苅田丈士
- Project Period (FY)
  2021 – 2023
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Review Section
  
  Basic Section 19020:Thermal engineering-related
- Research Institution
  Chubu University
Study of supersonic turbine with pseudo-shock modelPrincipal Investigator
- Principal Investigator
  
  Kanda Takeshi
- Project Period (FY)
  2018 – 2020
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Review Section
  
  Basic Section 19010:Fluid engineering-related
- Research Institution
  Chubu University

All 2021 2020 2018

All Journal Article Presentation

[Journal Article] A Way to Mitigate Force-Fight Oscillation Based on Pressure and Position Compensation for Fly-by-Wire Flight Control Systems2020
- Author(s)
  Takeshi KANDA and Kento HIKOSAKA
- Journal Title
  
  Trans. Japan Soc. Aero. S Sci.
  
  Volume: 63 Issue: 1 Pages: 1-7
- DOI
  10.2322/tjsass.63.1
- NAID
  130007779827
- ISSN
  0549-3811, 2189-4205
- Language
  English
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-18K03957
[Presentation] 超音速タービンの遠心力が翼列間流れに与える影響2021
- Author(s)
  稲垣達也、苅田丈士、中井亮夫
- Organizer
  日本機械学会 2021年度年次大会
- Data Source
  KAKENHI-PROJECT-18K03957
[Presentation] ロケットエンジンの高周波振動燃焼に関する研究2021
- Author(s)
  三品友揮、苅田丈士、村松駿太、早迫奨真
- Organizer
  機械学会2021年度年次大会
- Data Source
  KAKENHI-PROJECT-21K03925
[Presentation] 超音速タービン翼周りの流れの研究2020
- Author(s)
  中井亮夫、苅田丈士
- Organizer
  流体力学講演会／航空宇宙数値シミュレーション技術シンポジウム 2020オンライン
- Data Source
  KAKENHI-PROJECT-18K03957
[Presentation] 超音速タービン翼周りの流れの研究2020
- Author(s)
  浅野達郎、大熊康敬、苅田丈士、濱津正行、中村勝彦
- Organizer
  2019年度日本航空宇宙学会関西・中部支部合同秋期大会
- Data Source
  KAKENHI-PROJECT-18K03957
[Presentation] 拡大流路における擬似衝撃波の研究2018
- Author(s)
  彦坂健人、苅田丈士
- Organizer
  第55回日本航空宇宙学会中部・関西支部合同秋期大会
- Data Source
  KAKENHI-PROJECT-18K03957

Kanda Takeshi 苅田 丈士

Research Projects

Research Products

Study of High-Frequency Combustion Instability of Rocket Engines Based on Off-Design Combustion ModelPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Study of supersonic turbine with pseudo-shock modelPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

[Journal Article] A Way to Mitigate Force-Fight Oscillation Based on Pressure and Position Compensation for Fly-by-Wire Flight Control Systems2020

Author(s)

Journal Title

DOI

NAID

ISSN

Language

Data Source

[Presentation] 超音速タービンの遠心力が翼列間流れに与える影響2021

Author(s)

Organizer

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[Presentation] ロケットエンジンの高周波振動燃焼に関する研究2021

Author(s)

Organizer

Data Source

[Presentation] 超音速タービン翼周りの流れの研究2020

Author(s)

Organizer

Data Source

[Presentation] 超音速タービン翼周りの流れの研究2020

Author(s)

Organizer

Data Source

[Presentation] 拡大流路における擬似衝撃波の研究2018

Author(s)

Organizer

Data Source

Kanda Takeshi 苅田丈士