A turbulence transport model for the analysis of shock interface interactio
n-induced turbulent mixing is presented. Results given by the one-dimension
al (1-D) version of this model are compared with data obtained in shock-tub
e experiments. Calibrations are made from an air/He interface destabilized
by a 1.3 incident shock wave Mach number, taking into account the successiv
e interactions with the different reshocks on the shock tube end wall. Then
, using the same set of model constants, different gas pairs with both vari
ous Atwood and incident shock wave Mach numbers are considered, in order to
point out the influence of these main parameters on the results. Mixing zo
ne thickness time evolutions and 1-D density profiles are presented and dir
ectly compared with experimental results. Profiles of other variables such
as the space integral of the turbulent kinetic energy integral k dx, transl
ation energy integral rho u(x)(2) dx, and the ratio integral rho k dxl inte
gral rho u(x)(2) dx, given by the computations, are also shown. Using two d
ifferent initializations, in particular, to better describe the first phase
s of the phenomenon under study (i.e., taking into account the initial memb
rane in a horizontal shock tube configuration), we have found good agreemen
t between calculations and experiments. (C) 1999 American Institute of Phys
ics. [S1070-6631(99)00401-8].