Experimental results of surface pressure measurements on axisymmetric bodies in supersonic flows, which were obtained from 2003 to 2012, are summarized. It aims to improve numerical technique to predict laminar-turbulent transition in boundary layer with understanding of transition mechanism.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
超音速流中に置かれた軸対称物体の表面静圧変動
61881000.pdf
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