 |
 |
 |
|
|
|
[Sponsors] | ||||
September 17, 2006, 03:20
|
3D,analysis of NACA-0012,with WINGLET & non.
|
#1 |
|
Guest
Posts: n/a
|
I need an analysys of NACA 0012 Airfoil(chord=1 unit & SPAN =8 x chord) one time without any winglet.other time with very thin winglet(NACA 0012) installed at 90,115,125,135,145 degree ANGLE to outbord(for example the shape is for 135 deg = _____________/ & for 90 deg = _____________| ). (span of winglet is 0.5 chord of wing).upstrem velocity is 200 m/s. the output needed Cl-Cd at angle of attack between 0 to 10 degree & contour of velocity & pressure change in 3D & 2D. I need to ploting result.... PLEASE HELP ME,I have only 2 days time. PLEASE,PLEASE WITH BEST REGARDS THANK YOU
17 sep 2006 |
|
|
||
|
September 17, 2006, 09:59
|
Re: 3D,analysis of NACA-0012,with WINGLET & non.
|
#2 |
|
Guest
Posts: n/a
|
1 - open the software 2 - build the mesh 3 - define boundary conditions 4 - run the simulation 5 - post-process 6 - you've done your own job for once
|
|
|
|
||
|
September 17, 2006, 14:56
|
Re: 3D,analysis of NACA-0012,with WINGLET & non.
|
#3 |
|
Guest
Posts: n/a
|
No i have not any time I need a solved problem.!!! if you can help me please help,...... I have not any software for solving this problem. I don't how work with this software? PLEASE help me? THANK YOU
|
|
|
|
||
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| 3D,analysis of NACA-0012,with WINGLET & non. | SAEED MAHLOO | Phoenics | 4 | January 9, 2009 06:34 |
| 3D,analysis of NACA-0012,with WINGLET & non. | SAEED MAHLOO | CFX | 5 | September 22, 2006 14:13 |
| 3D,analysis of NACA-0012,with WINGLET & non. | SAEED MAHLOO | FLUENT | 0 | September 17, 2006 03:05 |
| 3D,analysis of NACA-0012,with WINGLET & non. | SAEED MAHLOO | FLUENT | 0 | September 17, 2006 03:04 |
| Naca 0012 | Arsineh Orland | Main CFD Forum | 1 | January 19, 2003 16:52 |
Linear Mode
