Supersonic combustion using multiple stinger-shaped injectors

Toshinori Kouchi, Sadatake Tomioka, Kohshi Hirano, Akiko Matsuo, Goro Masuya

Research output: Contribution to journalArticle

1 Citation (Scopus)
Original languageEnglish
Pages (from-to)56-59
Number of pages4
JournalTransactions of the Japan Society for Aeronautical and Space Sciences
Volume60
Issue number1
Publication statusPublished - 2017

Keywords

  • Combustor performance
  • Fuel mixing
  • Scramjet engine
  • Supersonic mixing and combustion

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Supersonic combustion using multiple stinger-shaped injectors. / Kouchi, Toshinori; Tomioka, Sadatake; Hirano, Kohshi; Matsuo, Akiko; Masuya, Goro.

In: Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 60, No. 1, 2017, p. 56-59.

Research output: Contribution to journalArticle

Kouchi, Toshinori ; Tomioka, Sadatake ; Hirano, Kohshi ; Matsuo, Akiko ; Masuya, Goro. / Supersonic combustion using multiple stinger-shaped injectors. In: Transactions of the Japan Society for Aeronautical and Space Sciences. 2017 ; Vol. 60, No. 1. pp. 56-59.
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