A Flux-Split Solution Procedure for Unsteady Inlet Flow Calculations
Keyword(s):
The solution of the reduced Navier Stokes (RNS) equations is considered using a flux-split procedure. Unsteady flow in a two dimensional engine inlet is computed. The problems of unstart and restart are investigated. A sparse matrix direct solver combined with a domain decomposition strategy is used to compute the unsteady flow field. Strong shock-boundary layer interaction, time varying shocks, and time varying recirculation regions are efficiently captured.
1998 ◽
Vol 371
◽
pp. 207-232
◽
1995 ◽
Vol 291
◽
pp. 369-392
◽
Keyword(s):
Keyword(s):
2008 ◽
Vol 614
◽
pp. 315-327
◽
Keyword(s):
1997 ◽