 |
 |
 |
|
|
|
[Sponsors] | ||||
December 19, 2002, 13:14
|
NACA 0012 pressure !!!!!!
|
#1 |
|
Guest
Posts: n/a
|
Dear all, I just made a program to simulate the pressure distribution around NACA 0012 based on artificial compressibility method. But my pressure distribution Cp(=-0.7) is higher than exp. data(=-1.2) around leading edge when Re=7.6*10^5,AOA=4 degree.I cannt find out why, anybody can help me this? Anyway, my result is good agreement with exp. data for AOA=0. Laminar and k-e model been tried,the mini grid distance on surface is about 0.001. Thanks help! Dexin
|
|
|
||
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| NACA 0012 Experimental Data | prasad84 | Main CFD Forum | 19 | February 22, 2023 10:03 |
| How to import NACA 0012 Profile in Gridgen | maplepink | Main CFD Forum | 17 | May 7, 2013 14:01 |
| Neumann pressure BC and velocity field | Antech | Main CFD Forum | 0 | April 25, 2006 03:15 |
| NACA 0012 simulation results | Luis | FLUENT | 3 | February 15, 2006 12:42 |
| Hydrostatic pressure in 2-phase flow modeling (CFX4.2) | HB &DS | CFX | 0 | January 9, 2000 14:19 |
Linear Mode
