The attemperator of the gas bypass of Jiawang PFBC-CC pilot plant was studied by simulating experiment and numerical calculation.
采用冷态模拟实验与数值计算相结合的方法对贾汪pfbc CC中试电站旁路烟道的减温器进行了专门研究设计。
The aim of numerical experiment of ram air turbines is mainly to simulating its adjustable pitch aerodynamic characteristic on the actual flight refuel conditions.
冲压空气涡轮流场数值研究主要目的是模拟在实际高空加油工作状态下涡轮变桨距气动特性。
Numerical simulating analysis of the main experiment results has been accomplished by use of RETRAN 02 code.
然后应用RETRAN02程序完成主要实验工况数值模拟计算。
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