We formulate a lattice Boltzmann model to solve supersonic flows. The parti
cle velocities are determined by the mean velocity and internal energy. The
adaptive nature of particle velocities permits the mean flow to have a hig
h Mach number. The introduction of a particle potential energy causes the m
odel to be suitable for a perfect gas with an arbitrary specific heat ratio
. The macroscopic conservation equations are derived by the Chapman-Enskog
method. The simulations were carried out on the hexagonal lattice. However,
the extension to both two- and three-dimensional square lattices is straig
htforward. As preliminary tests, we present the Sod shock-tube simulation a
nd the two-dimensional shock reflection simulation. [S1063-651X(98)15911-1]
.