Parametric study of airframe-integrated scramjet cooling requirement

Takeshi Kanda, Goro Masuya, Yoshio Wakamatsu, Nobuo Chinzei, Akio Kanmuri

Research output: Contribution to journalArticle

32 Citations (Scopus)

Abstract

In a previous report, scramjet engine characteristics of different propellant-fed cycles were compared and engine performances were discussed. In this study, the cooling requirement of a hydrogen-fueled airframe-integrated scramjet engine as well as an airframe was examined, and effects of various parameters including flight Mach number, flight dynamic pressure, engine wall temperature, and engine scale, on the engine characteristics were analyzed. The coolant required for the airframe was about 20% of the total coolant. Simple equations that correlate coolant flow rate with those parameters were derived.

Original languageEnglish
Pages (from-to)431-436
Number of pages6
JournalJournal of Propulsion and Power
Volume7
Issue number3
DOIs
Publication statusPublished - 1991 Jan 1

ASJC Scopus subject areas

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

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  • Cite this

    Kanda, T., Masuya, G., Wakamatsu, Y., Chinzei, N., & Kanmuri, A. (1991). Parametric study of airframe-integrated scramjet cooling requirement. Journal of Propulsion and Power, 7(3), 431-436. https://doi.org/10.2514/3.23344