http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
study of numerical methods to solve quasi one-dimensional, unsteady, compressible viscous flow with shock
xiv, 137 leaves : illustrations ; 28 cm.
case, upon a McCormack predictor-corrector scheme are
consitions are considered, to simulate highly unsteady
developed. Comparison between the inviscid flow and the
flows. The advantages of this method, in this particular
influence when the geometry of the nozzle is too large.
internal flow in a subsonicsupersonic nozzle is obtained.
inviscid and viscous flows, using an original two point
Shocks due to high pressure ratio are computed for both
subsonic-supersonic solving algorithm. Unsteady boundary
The numerical simulation of a quasi one-dimensional
viscous flow shows that the viscous effect have little
"Major subject: Mechanical Engineering ".