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Fingerprint Dive into the research topics where Tetsuya Satou is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

Turbojet engines Engineering & Materials Science
Engines Engineering & Materials Science
engine Earth & Environmental Sciences
turbojet engines Physics & Astronomy
engines Physics & Astronomy
Hypersonic aerodynamics Engineering & Materials Science
Mach number Engineering & Materials Science
Wind tunnels Engineering & Materials Science

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Research Output 1995 2019

  • 405 Citations
  • 11 h-Index
  • 45 Conference contribution
  • 28 Article
  • 3 Paper
  • 2 Chapter
1 Citation (Scopus)

Investigation of cryogenic chilldown in a complex channel under low gravity using a sounding rocket

Kinefuchi, K., Sarae, W., Umemura, Y., Fujita, T., Okita, K., Kobayashi, H., Nonaka, S., Himeno, T. & Satou, T., 2019 Jan 1, In : Journal of Spacecraft and Rockets. 56, 1, p. 91-103 13 p.

Research output: Contribution to journalArticle

Sounding rockets
sounding rockets
microgravity
Cryogenics
cryogenics
1 Citation (Scopus)

Investigation of the void fraction–quality correlations for two-phase hydrogen flow based on the capacitive void fraction measurement

Sakamoto, Y., Kobayashi, H., Naruo, Y., Takesaki, Y., Nakajima, Y., Furuichi, A., Tsujimura, H., Kabayama, K. & Sato, T., 2019 Jul 5, In : International Journal of Hydrogen Energy. 44, 33, p. 18483-18495 13 p.

Research output: Contribution to journalArticle

Void fraction
voids
Hydrogen
hydrogen
Boiling liquids

A study on time evolution method for hyperbolic navier-stokes system

Nagao, T., Hashimoto, A. & Satou, T., 2018 Jan 1, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Advection
Laminar flow
Aspect ratio
Computational fluid dynamics
Reynolds number

Experimental study of delaying effect of the frost formation on cryogenic heat exchanger tube surfaces using super-hydrophobicity tube by anodic oxidation method

Tokawa, S., Kinoshita, Y., Kurata, T., Osumi, R. & Satou, T., 2018 Jan 1.

Research output: Contribution to conferencePaper

tube heat exchangers
frost
Tubes (components)
Anodic oxidation
turbojet engines

Numerical simulation of the side-clearance effect on the supersonic air-inlet performance for high mach integrated control experiment “himico

Sano, M., Yoshida, H., Wakabayashi, S., Chiga, T., Satou, T., Hashimoto, A. & Kojima, T., 2018 Jan 1, 2018 Joint Propulsion Conference. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-4539. (2018 Joint Propulsion Conference).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Integrated control
Flow separation
Air intakes
Mach number
Computer simulation