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A method for computing the mole fraction of Carbon monoxide in a liquid propellant engine

عنوان مقاله: A method for computing the mole fraction of Carbon monoxide in a liquid propellant engine
شناسه ملی مقاله: ISPTC18_262
منتشر شده در هجدهمین همایش شیمی فیزیک ایران در سال 1394
مشخصات نویسندگان مقاله:

A.R Roudbari - Department of Aerospace, Shahid Sattari University, Tehran, Iran
M Norouzi Bakhsh - Department of Aerospace, Shahid Sattari University, Tehran, Iran

خلاصه مقاله:
Analysis of combustion products and combustion condition such as oxidizer to fuel ratio,combustion chamber pressure and environmentally consideration ,thrust profile are one of theimportant section off accept or reject of the fuel. One of the pollutant gases are Carbonemonoxide, so we want to find a reliable relation for analysis mole fraction of Carbonemonoxide in combustion of liquid butane and liquid oxygen by special software in highpressure.

صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/552721/