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Mach number study of supersonic turbulence: the properties of the density field
Ist Teil von
Monthly notices of the Royal Astronomical Society, 2016-08, Vol.460 (4), p.4483-4491
Ort / Verlag
London: Oxford University Press
Erscheinungsjahr
2016
Quelle
Alma/SFX Local Collection
Beschreibungen/Notizen
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 (
$\mathcal {M} \approx 0.5$
) to the highly supersonic regime (
$\mathcal {M}\approx 16$
). The forcing scheme consists of both solenoidal (transverse) and compressive (longitudinal) modes in equal parts. We confirm the relation
$\sigma _{s}^2 = \ln {(1+b^2\mathcal {M}^2)}$
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
$\mathcal {D}(k,\,\mathcal {M}) \propto k^{\zeta (\mathcal {M})}$
with scaling exponents depending on the Mach number. We find
$\zeta (\mathcal {M}) = \alpha \mathcal {M}^{\beta }$
with coefficients α = −2.1 and β = −0.33. The dependence of the scaling exponent on the Mach number implies a fractal dimension
$D=2+1.05 \mathcal {M}^{-0.33}$
.