Study of Equivalence Ratio and Propellant Effects on a Reactive Flow with Low Residence Time and Highly Variable Tempereture and Pressure

امیر مردانی, محمدصالح عبداله پور, محمدصالح, رضائی - Fuel and Combustion, 2014‎ - jfnc.ir
Gas aerothermodynamics is the thermodynamics of a gas in high velocity associated with
heat transfer. One of the devices which takes advantage of this field is a rocket system. High
velocity flow filedwith intensely varying pressure and temperature along the nozzle axis
leads to reduction ofresidence time. This means the balance between chemical and flow
time scales is changing in the flow stream. In this study, reacting flow composition variations
in combustion chamber and nozzle of a liquid rocket engine is numerically investigated for …
以上显示的是最相近的搜索结果。 查看全部搜索结果