日本機械学会論文集 B編
Online ISSN : 1884-8346
Print ISSN : 0387-5016
直接数値シミュレーションによる超音速混合層の大規模構造
藤田 雅司前川 博
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ジャーナル フリー

1994 年 60 巻 574 号 p. 2052-2057

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In the present paper, coherent structures of the supersonic mixing layer are investigated by direct numerical simulations of a spatialy developing free shear layer, We examined numerical results of the velocity components, u, v, w simulated by Fouillet and Lesieur : Reynolds number Re=δω0ΔU/ν=1500, Mach number =1(M1=1 and Mc=0.3), (U1+U2)/2=0.7, U1-U2=0.6, and the hyperbolic-tangent velocity profile is perturbed by weak three-dimensional white noise. We find that the coherent structures in the supersonic mixing layer at Mc=0.3 are three dimensional and have rib structures with strong vorticities of ωy and ωx similar to those in the incompressible mixing layer. The helical pairing structures found in the rib structure generate a coherent 'upwash' and 'downwash' fluid motion in the supersonic mixing layer. The regions corresponding to high rates of dissipation are found in the rib structures.

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