在空气循环子系统中，各状态点的温度都随飞行高度的增加而减小。
In the subsystem of air cycle, temperature in all state points decreases with the increasing altitude.
研究表明在完全循环加载过程中，由于残余应变的存在，马氏体相变应力随循环增加而减小。
The research results show martensite transformation stress decreases with an increase in cycle due to the residual strain during full cyclic loading.
进气量固定时，随循环压力的增加而逐渐减小。
When the air intake quantity was fixed, the air content ratio would be reduced with the circulated pressure increased.
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