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2017 Fiscal Year Final Research Report

Two-color PLIF Measurement of Instantaneous Molar Fraction in A Supersonic Combustor

Research Project

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Project/Area Number 15H04199
Research Category

Grant-in-Aid for Scientific Research (B)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionOkayama University

Principal Investigator

Kouchi Toshinori  岡山大学, 自然科学研究科, 准教授 (40415922)

Co-Investigator(Kenkyū-buntansha) 柳瀬 眞一郎  岡山大学, 自然科学研究科, 教授 (20135958)
永田 靖典  岡山大学, 自然科学研究科, 助教 (20635594)
Project Period (FY) 2015-04-01 – 2018-03-31
Keywords先端レーザー計測 / 超音速混合・燃焼 / 推進工学 / 圧縮性流体
Outline of Final Research Achievements

Spaceplane is a promising candidate for next generation space transportation system. Supersonic mixing and combustion are keys to realize the spaceplane. We developed a new technique to measure instantaneous injectant molar fraction in a supersonic flow through this project. The measurement technique is based on Planner Laser Induced Fluoresces (PLIF) using tracer molecules which are excited by laser light. To establish the technique, we first investigated photochemical characteristics of toluene under low-temperature and pressure conditions which is observed in a suction-type supersonic wind tunnel. Then, we established the two-color PLIF measurement system. By using this new measurement system, we are able to quantitatively evaluate mixing efficiency of fuel in a supersonic flow.

Free Research Field

推進工学

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Published: 2019-03-29  

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