The thermal shock resistance of plasma-sprayed ZrO2 thermal barrier coatings under the conditions of water quenching and flamejet was studied.
研究了涂层在水淬和火焰喷烧两种条件下的抗热震性能。
2
In order to achieve a rapid initiation of detonation in a short distance, a flamejet ignition system was applied to the pulse detonation rocket engine (PDRE).
为了实现快速短距起爆，火焰射流点火系统被尝试应用在脉冲爆震火箭发动机上。
3
The principle of the method and its calculation processes are discussed, and results of a stable jetflame temperature distribution are given.