Physical interactions between turbulence and shock waves are very comp
lex phenomena. If these interactions take place in chemically reacting
flows, the degree of complexity increases dramatically. Examples of a
pplications may be cited in the area of supersonic combustion, in whic
h the controlled generation of turbulence and/or large scale vortices
in the mixing and flame-holding zones is crucial for efficient combust
ion. Equally important, shock waves interacting with turbulence and ch
emical reactions affect the combustor flowfield resulting in enhanced
relaxation and chemical reaction rates. Chemical reactions in turn con
tribute to dispersion of shock waves and reduction of turbulent kineti
c energies. Computational schemes to address these physical phenomena
must be capable of resolving various length and time scales. These sca
les are widely disparate and the most optimum approach is found in exp
licit/implicit adjustable schemes for the Navier-Stokes solver. This i
s accomplished by means of the generalized Taylor-Galerkin (GTG) finit
e element formulations. Adaptive meshes are used in order to assure ef
ficiency and accuracy of solutions. Various benchmark problems are pre
sented for illustration of the theory and applications. Geometries of
ducted rockets, supersonic diffusers, flame holders, and hypersonic in
lets are included. Merits of proposed schemes are demonstrated through
these example problems.