|
[Sponsors] |
[Other] Definition of the NACA 65 on the bladegen |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
March 30, 2010, 08:26 |
Definition of the NACA 65 on the bladegen
|
#1 |
Member
Domenico
Join Date: Sep 2009
Location: Cranfield
Posts: 48
Rep Power: 17 |
Dear all,
I 'm generating the blade geometry through BLADEGEN software, and in particular I'm studying a compressor fan where the profile of its rotor and stator are NACA 65. Then I want to implement that information on the BLADEGEN, but by using the NACA thickness dialog window I can specify some other parameters. However I can't define the designation on the same window. Please, let me know as soon as possible. P.s. You can have look on the attached file Kind regards Domenico di Cugno |
|
March 8, 2013, 02:55 |
|
#2 |
New Member
Anonymous
Join Date: Mar 2013
Posts: 4
Rep Power: 13 |
Hi Domenico,
Although Im sorry i cant answer your question. I'm hoping you can help me. Im still new to ANSYS and I cant seem to find the dialog thickness window. Could you help? Thanks |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
BladeGen problem | David Wang | CFX | 5 | April 2, 2016 06:18 |
Theta angle definition in BladeGen | Raul | CFX | 2 | November 1, 2012 12:02 |
OpenFOAM14 for Mac OSX Darwin 104 | gschaider | OpenFOAM Installation | 118 | July 20, 2008 06:19 |
Ansys CFX Vs. NACA Summary Report. Mismatch Result | Santiago Orrego. | CFX | 3 | February 5, 2007 13:05 |
bladegen & NACA profile | ichgut | CFX | 1 | August 9, 2004 10:31 |