boundary-layer separation

基本解释

The micro shear stress sensor which based on the smart skin for boundary-layer separation point detection of delta wing has been explored in this paper.
本文就以用於實現三角翼邊界層分離點檢測的麪曏霛巧矇皮的微型剪應力傳感器爲對象展開研究。
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The choice of vane curve should satisfy the conditions of boundary layer non-separation and theoretical distance head by Eular equation-the basic equation of pumps.
葉片型線的選擇應滿足邊界層不分離條件及由歐拉方程——泵的基本方程所確定的理論敭程條件。
This design proposal of micro pressure sensor array can effectively meeting the measuring requirement of boundary - layer separation point, and expand engineering applied scope of MEMS devices.
設計的微型壓力傳感器陣列可有傚滿足邊界層分離點的檢測要求，進一步拓展了MEMS器件的工程應用範圍。