inlet total pressure recovery的意思|示意
进气道总压恢复
inlet total pressure recovery的网络常见释义
进气道总压恢复 定义 中文名称： 进气道总压恢复 英文名称： inlet total pressure recovery 其他名称： 进气扩压效率 定义： 进气道出口气瓶总压与远前方来流总压之比值。 应用学科： 航空科技（一级学科）；推进技术与航空动力装置（二级学科） 本 基于1
inlet total pressure recovery相关例句
By comparison of inlet total pressure recovery coefficient, attack-angle performance of chin inlet and two-dimensional inlet are superior to frontal inlet.
对不同布局的总压恢复系数进行比较，颌下及两侧进气则较头部进气有好的攻角特性。
And three-dimensional sidewall compression inlet with 25 percent cowl position has high mass capture and total pressure recovery coefficient and isolator exit flow flied is homogeneous.
整流罩位置为25%的三维侧压进气道可以获得较高质量捕获和总压恢复系数，且隔离段出口流场比较均匀。
Changes of sidewall sweep Angle and cowl position can influence inlet performance such as mass capture, total pressure recovery coefficient and uniformity of isolator exit flow field.
侧板后掠角大小和整流罩位置变化时，对进气道的质量捕获、总压恢复系数和隔离段出口流场的均匀性等都有一定的影响。
The results show that this type of inlet has high total pressure recovery coefficients at a wide range of yaw angle.
研究表明，该类进气道在各种侧滑状态下总压恢复系数较高。