The time-dependent Transonic Small Disturbance equation, will be reformulated in Hyperbolic Conservation Law form. In Hyperbolic Conservation Law form, with dimensional splitting the equations can be discretized and treated as a series of Riemann problems. Steady subsonic and transonic flow calculations will be presented for a suitable test configuration and where possible comparisons will be made with analytic solutions.
@article{620,
title = {Transonic flow calculations using a dimensional splitting method},
journal = {ANZIAM Journal},
volume = {42},
year = {2000},
doi = {10.21914/anziamj.v42i0.620},
language = {EN},
url = {http://dml.mathdoc.fr/item/620}
}
Hung, Hing; Gear, John A.; Phillips, Natalie J. T. Transonic flow calculations using a dimensional splitting method. ANZIAM Journal, Tome 42 (2000) . doi : 10.21914/anziamj.v42i0.620. http://gdmltest.u-ga.fr/item/620/