Mach number study of supersonic turbulence: The properties of the density field

31Citations
Citations of this article
27Readers
Mendeley users who have this article in their library.

This article is free to access.

Abstract

We analyse the scaling properties of turbulent flows using a suite of three-dimensional numerical simulations. We model driven, compressible, isothermal, turbulence with Mach numbers ranging from the subsonic (ℳ ≈ 0.5) to the highly supersonic regime (ℳ ≈ 16). The forcing scheme consists of both solenoidal (transverse) and compressive (longitudinal) modes in equal parts. We confirm the relation σs2 = ln (1 + b2 ℳ2) between the Mach number and the standard deviation of the logarithmic density with b = 0.33. We find increasing deviations with higher Mach number from the predicted lognormal shape in the high-density wing of the density probability density function. The density spectra follow D{script}(k, ℳ) ∝ kζ(ℳ) with scaling exponents depending on the Mach number. We find ζ(ℳ) = αℳβ with coefficients α = -2.1 and β = -0.33. The dependence of the scaling exponent on the Mach number implies a fractal dimension D = 2 + 1.05 ℳ-0.33.

Cite

CITATION STYLE

APA

Konstandin, L., Schmidt, W., Girichidis, P., Peters, T., Shetty, R., & Klessen, R. S. (2016). Mach number study of supersonic turbulence: The properties of the density field. Monthly Notices of the Royal Astronomical Society, 460(4), 4483–4491. https://doi.org/10.1093/mnras/stw1313

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free