Computational analysis of the unsteady flow induced by adouble-wedge shaped projectile overtaking shock waves[J]. ACTA AERODYNAMICA SINICA, 2002, 20(3): 260-266.
Citation: Computational analysis of the unsteady flow induced by adouble-wedge shaped projectile overtaking shock waves[J]. ACTA AERODYNAMICA SINICA, 2002, 20(3): 260-266.

Computational analysis of the unsteady flow induced by adouble-wedge shaped projectile overtaking shock waves

  • loading

Catalog

    Turn off MathJax
    Article Contents

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return