|
[Sponsors] |
April 21, 2006, 09:47 |
subsonic nozzle flow, inlet-outlet BCs
|
#1 |
Guest
Posts: n/a
|
Hi all, about the choice of the inlet-outlet BCs for a subsonic compressible nozzle flow is a difficulty puzzling me. And the non reflecting conditions presented by David H. Rudy and the NSCBC presented by S.K. Lele appear not obviously suitable for the probleme of this type.Any help is greatly appreciated. Best regards
|
|
May 8, 2006, 13:59 |
Re: subsonic nozzle flow, inlet-outlet BCs
|
#2 |
Guest
Posts: n/a
|
At the inflow, characteristic analysis dictates that the transverse velocities be specified (usually zero). Two variables from the group density, temp, and longitudinal velocity must also be specified, and one variable (usually longitudinal velocity) must be allowed to float.
At the outflow, the transverse and longitudinal velocities, as well as density, are allowed to float. Temperature is specified. Often, pressure is specified, which in turn leads to specifying temperature after calculating density. These conditions will reflect accoustic waves. For non-reflecting conditions, your best bet is to follow the work of Kevin Thompson and Poinsot and Lele. |
|
May 15, 2006, 11:33 |
Re: subsonic nozzle flow, inlet-outlet BCs
|
#3 |
Guest
Posts: n/a
|
Hi, You can also follow Francois Dubois recipes according which the problem is well posed if: 1) for inlet boundary the density and temperature is given; 2) for outlet boundary there are two cases: 2.1) subsonic outlet BC => static pressure has to be given; 2.2) supersonic outlet BC => no datum has to be prescribed. All above is related to Riemann problem solution between boundary manifold and state. Happy coding!
|
|
May 15, 2006, 11:37 |
Re: subsonic nozzle flow, inlet-outlet BCs
|
#4 |
Guest
Posts: n/a
|
Also, be advised - you have to solve linearised Riemann problem, so, in case of subsonic outlet, the prescribed static pressure has to be close enough to that one in the last cell...
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Laval Nozzle sonicFoam inlet and outlet bc | BernhardGrieser | OpenFOAM Running, Solving & CFD | 10 | February 16, 2017 08:45 |
Mass flow inlet and pressure outlet issue | nikhil | FLUENT | 5 | December 11, 2013 13:30 |
inlet and outlet for convergent nozzle | josh99 | FLUENT | 1 | December 25, 2011 14:24 |
UDF for transient pressure inlet, mass flow check at nozzle exit and volumetric heat | kokoory | FLUENT | 0 | August 17, 2011 03:07 |
Subsonic flow in a supsersonic nozzle | Laplacien | FLUENT | 0 | April 6, 2006 04:27 |