The computational qualities of spatially high-order accurate methods f
or the finite-volume solution of the Euler equations are presented. Mu
ltidimensional reconstruction operators discussed include versions of
the k-exact and essentially nonoscillatory (ENO) algorithms. The ENO s
chemes utilized are the reconstruction-via-primitive-function scheme a
nd a dimensionally split ENO reconstruction. High-order operators are
compared in terms of reconstruction and solution accuracy, computation
al cost, and oscillatory behavior in supersonic flows with shocks. Inh
erent steady-state convergence difficulties are demonstrated for the i
mplemented adaptive-stencil algorithms. An exact solution to the heat
equation is used to determine reconstruction error, and the computatio
nal intensity is reflected through operation counts. The standard vari
able-extrapolation method (MUSCL) is included for comparison. Numerica
l experiments include the Ringleb flow for numerical accuracy and a sh
ock-reflection problem. A vortex-shock interaction demonstrates the ab
ility of the ENO scheme to excel in simulating unsteady high-frequency
flow physics.