에탄올 점화 과정에 관한 충격관 실험 및 모델 연구

Shock Tube and Modeling Study of Ethanol Ignition

초록

The ignition of ethanol-oxygen-argon mixture was studied in reflected shock waves over the tem-perature range of 1281-1625 K and the pressure range of 0.69-1.06 bar. The ignition delay time was measured by thesudden increase of pressure profile and the radiation emitted by OH radicals. The relationship between the ignition delaytime and the concentrations of ethanol and oxygen was determined in the form of mass-action expressions with an Arrhe-nius temperature dependence. In contrast to the behavior observed in methanol, ethanol acts to inhibit rather than accel-erate its own ignition. Several kinetic mechanisms proposed for ethanol oxidation at high temperatures have been testedby the computer simulation.

키워드

EthanolIgnition Delay TimeShock tubeCombustion MechanismEthanolIgnition Delay TimeShock tubeCombustion Mechanism
제목
에탄올 점화 과정에 관한 충격관 실험 및 모델 연구
제목 (타언어)
Shock Tube and Modeling Study of Ethanol Ignition
저자
신권수박기수권은숙
발행일
2004-02
저널명
대한화학회지
48
1
페이지
12 ~ 16