Citation:
Huete, C., Velikovich, A. L., Martínez-Ruiz, D., & Calvo-Rivera, A. (2021). Stability of expanding accretion shocks for an arbitrary equation of state. Journal of Fluid Mechanics, 927(A35)
xmlui.dri2xhtml.METS-1.0.item-contributor-funder:
Ministerio de Ciencia e Innovación (España)
Sponsor:
C.H. work is produced with the support of a 2019 Leonardo Grant for Researchers and Cultural Creators, BBVA Foundation and project PID2019-108592RB-C41 (MICINN/FEDER, UE). A.L.V. work was supported by the National Nuclear Security Administration of the U.S. Department of Energy. D.M-R work was supported by project PID2019-108592RA-C43 (MICINN/FEDER, UE).
Project:
Gobierno de España. PID2019-108592RB-C41 Gobierno de España. PID2019-108592RA-C43
Keywords:
Gas dynamics
,
Shock waves
,
Supersonic flow
We present a theoretical stability analysis for an expanding accretion shock that does
not involve a rarefaction wave behind it. The dispersion equation that determines the
eigenvalues of the problem and the explicit formulae for the corresponding eigenfunctWe present a theoretical stability analysis for an expanding accretion shock that does
not involve a rarefaction wave behind it. The dispersion equation that determines the
eigenvalues of the problem and the explicit formulae for the corresponding eigenfunction
profiles are presented for an arbitrary equation of state and finite-strength shocks.
For spherically and cylindrically expanding steady shock waves, we demonstrate the
possibility of instability in a literal sense, a power-law growth of shock-front perturbations
with time, in the range of hc < h < 1 + 2M2, where h is the D’yakov-Kontorovich
parameter, hc is its critical value corresponding to the onset of the instability and M2
is the downstream Mach number. Shock divergence is a stabilizing factor and, therefore,
instability is found for high angular mode numbers. As the parameter h increases from hc to 1 + 2M2, the instability power index grows from zero to infinity. This result contrasts
with the classic theory applicable to planar isolated shocks, which predicts spontaneous
acoustic emission associated with constant-amplitude oscillations of the perturbed shock in the range hc < h < 1 + 2M2. Examples are given for three different equations of state: ideal gas, van der Waals gas and three-terms constitutive equation for simple metals.[+][-]