|
[Sponsors] |
October 12, 2000, 08:53 |
Verification of Supersonic Nozzle Flow
|
#1 |
Guest
Posts: n/a
|
Hello CFD Users,
I am trying to analyse flow through supersonic de-Laval Nozzle at inlet condition of 8 bars, the fluid at present being used is AIR. This gives me an exit Mach No. approx. 2.06, which correlates with the one-dimensional theory. But I am not too sure whether results Y+ values along the expansion section wall is right? The wall velocity distribution theory suggests that, for a laminar flow Y+ < 11.63 & for a turbulent flow Y+ > 11.63. The result that am getting are Y+ >1<5 for very fine grids near the wall, Y+ >2<10 for medium size grids and Y+ >5<15 for very large grid size. Is there any CFD user, who has delth with supersonic flow in NOzzles or any of you who know more about this phenomena. Can you please help ? PS - The turbulent model that I have used for this situation is k-epsilon Realisable, with near wall treatment as Non-Equilibium Wall functions in FLUENT 5.3. Would I be right to use this particular model or through your experience, better model exists. Can you suggest. Thank you very much for you time and effort Ali Khan |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Nozzle Flow - Divergence Problem | Ijaz | FLUENT | 9 | January 11, 2014 05:36 |
Flow in Supersonic MHD Channel | Antanas | CFX | 6 | February 13, 2012 15:49 |
UDF for transient pressure inlet, mass flow check at nozzle exit and volumetric heat | kokoory | FLUENT | 0 | August 17, 2011 03:07 |
Compressible de Laval Nozzle Flow | rw511 | CFX | 3 | May 22, 2011 20:48 |
Flow simulation in a Pelton turbine nozzle | fivos | FLUENT | 0 | April 19, 2011 12:46 |