|
[Sponsors] |
Dynamic pressure at stag point for 3d aerofoil |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
January 25, 2006, 19:59 |
Dynamic pressure at stag point for 3d aerofoil
|
#1 |
Guest
Posts: n/a
|
hi all, im modeeling flow around a 3d aerofoil section. at the stagnation point on the leading edge, fluent reads that velocity is zero as expected. however it also tells me that local dynamic pressure at the same point is +27Pa. this is completely baffling me. if anyone has any ideas they would be greatly appreciated. thanks
|
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Pulsatile pressure inlet with pressure outlet | a.lynchy | FLUENT | 3 | March 23, 2012 13:45 |
Dynamic Pressure Formula and Distribution | AK | FLUENT | 2 | January 3, 2004 01:53 |
what the result is negatif pressure at inlet | chong chee nan | FLUENT | 0 | December 29, 2001 05:13 |
Pressure boundary condition | Brindaban Ghosh | Main CFD Forum | 6 | May 3, 2000 13:11 |
Hydrostatic pressure in 2-phase flow modeling (long) | DS & HB | Main CFD Forum | 0 | January 8, 2000 15:00 |