研究了涂层在水淬和火焰喷烧两种条件下的抗热震性能。
The thermal shock resistance of plasma-sprayed ZrO2 thermal barrier coatings under the conditions of water quenching and flame jet was studied.
对航天飞行器防热部件在氧煤油发动机火焰喷吹下的烧蚀行为进行了有限元数值模拟。
The ablation behavior of spacecraft thermo-resistance components under blowing by oxygen-kerosene flame is investigated by means of finite element numerical simulation.
配制系列高炉喷补料，并检测其烧后线变化及耐热震性等性能。
Gunning refractory are made and its properties, such as linear change during baking and thermal shock resistance, are measured.
应用推荐