flow total造句

• The effects of such elements as primary flow total pressure, flow rate, degree of fuel rich, nozzle structure, flying speed and secondary combustion on ejecting mode performance were researched . it was found that thrust augmentation can be achieved on the condition that the flying mach number is above 0.7 . to deeply analyze thrust augmentation mechanism in low speed range, the research was further continued by changing secondary combustion organization and aft-body configuration
  研究了一次流总压、流量、富燃程度、喷管结构、二次流来流速度、二次燃烧组织对引射模态性能的影响，发现实验样机构型在0.7ma以上的飞行条件下可以获得推力增强，而在0.7ma以下无推力增强。