Souri, Hossein

[ 1 ] - بررسی خواص ترموفیزیکی سوخت کروسینی حاوی نانولوله کربنی برای خنک کاری محفظه احتراق راکت

The engine cooling in first stage of satellite carrier rocket via kerosene fuel leads to increase the missile range. For increasing the heat transfer coefficient of the fuel, addition of nanoparticle is a preferred method. At constant velocity of nanofuel through the fuel flow passage in combustion chamber, evaluation of the coefficient depends on assessment of the effective parameters. These p...