文件名称:external_compressible
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问题考虑围绕翼型的流动在4°攻角和一个自由流马赫数0.8。流量是跨音速，并有近于上（吸气）侧中间弦m/c=0.45一个相当强烈的震撼。弦长为1米。-The problem considers the flow around an airfoil at an angle of attack and a free stream Mach number of ( ). The flow is transonic, and has a fairly strong shock near the mid-chord ( ) on the upper (suction) side. The chord length is 1 m.
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下载文件列表
external_compressible\airfoil-1.cas.gz
.....................\airfoil-1.dat.gz
.....................\airfoil-2.cas.gz
.....................\airfoil-2.dat.gz
.....................\airfoil.cas.gz
.....................\airfoil.dat.gz
.....................\airfoil.msh
.....................\cd-history
.....................\cl-history
.....................\cm-history
.....................\monitor-1.out
external_compressible