EI、Scopus 收录
中文核心期刊
CROSSFLOW INSTABILITY OF HIGH SPEED THREE DIMENSIONAL BOUNDARY LAYER 1)[J]. Chinese Journal of Theoretical and Applied Mechanics, 1998, 30(5): 521-530. DOI: 10.6052/0459-1879-1998-5-1995-158
Citation: CROSSFLOW INSTABILITY OF HIGH SPEED THREE DIMENSIONAL BOUNDARY LAYER 1)[J]. Chinese Journal of Theoretical and Applied Mechanics, 1998, 30(5): 521-530. DOI: 10.6052/0459-1879-1998-5-1995-158

CROSSFLOW INSTABILITY OF HIGH SPEED THREE DIMENSIONAL BOUNDARY LAYER 1)

  • There exist variety of instability in three dimensional boundary layer on swept wing, the cross-flow instability is dominant The flow over rotating cone is typical three dimensional boundary layer It has been shown that the experimental and theoretical results of rotating cone can be used to model cross flow instability of swept wing At high speeds, where even the basic flow calculations of swept wing are a problem, owe to it′s simple geometry, rotating cone become a suitable and valuable model to ...
  • loading

Catalog

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return