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