Ss. Lee et al., DIRECT NUMERICAL-SIMULATION OF ISOTROPIC TURBULENCE INTERACTING WITH A WEAK SHOCK-WAVE, Journal of Fluid Mechanics, 251, 1993, pp. 533-562
Interaction of isotropic quasi-incompressible turbulence with a weak s
hock wave was studied by direct numerical simulations. The effects of
the fluctuation Mach number M(t) of the upstream turbulence and the sh
ock strength M1(2)-1 on the turbulence statistics were investigated. T
he ranges investigated were 0.0567 less-than-or-equal-to M(t) less-tha
n-or-equal-to 0.110 and 1.05 less-than-or-equal-to M1 less-than-or-equ
al-to 1.20. A linear analysis of the interaction of isotropic turbulen
ce with a normal shock wave was adopted for comparisons with the simul
ations. Both numerical simulations and the linear analysis of the inte
raction show that turbulence is enhanced during the interaction with a
shock wave. Turbulent kinetic energy and transverse vorticity compone
nts are amplified, and turbulent lengthscales are decreased. The predi
ctions of the linear analysis compare favourably with simulation resul
ts for flows with M(t)2 < a(M1(2)-1) with a almost-equal-to 0.1, which
suggests that the amplification mechanism is primarily linear. Simula
tions also showed a rapid evolution of turbulent kinetic energy just d
ownstream of the shock, a behaviour not reproduced by the linear analy
sis. Investigation of the budget of the turbulent kinetic energy trans
port equation shows that this behaviour can be attributed to the press
ure transport term. Shock waves were found to be distorted by the upst
ream turbulence, but still had a well-defined shock front for M(t)2 <
a(M1(2)-1) with a almost-equal-to 0.1). In this regime, the statistics
of shock front distortions compare favourably with the linear analysi
s predictions. For flows with M(t)2 > a(M1(2)-1) with a almost-equal-t
o 0.1, shock waves no longer had well-defined fronts: shock wave thick
ness and strength varied widely along the transverse directions. Multi
ple compression peaks were found along the mean streamlines at locatio
ns where the local shock thickness had increased significantly.