|
[Sponsors] |
June 13, 2012, 16:53 |
Naca0012 simulation data
|
#1 |
Member
mahzad_kh
Join Date: Jun 2010
Posts: 38
Rep Power: 16 |
Hi every one!
I've written a 2D incompressible finite volume code for the computation of laminar low Re flow passing airfoils! I didn't use turbulence modeling, and I just want to model low Re, incompressible fully laminar flows, I mean(100<Re<10000). I'd searched for some data of naca 0012 (in case of incidence), but the problem is that I couldn't find any experimental or numerical data to validate my results! So How can I get the reference values of naca 0012 for this sort of very low Reynolds laminar flow ? Does anyone knows any paper or thesis which can help me with my problem? can anybody share experiences about validating results in this type of low Re flow? Thanks for any words in advance! |
|
June 13, 2012, 22:11 |
|
#2 |
Senior Member
Mehdi Babamehdi
Join Date: Jan 2011
Posts: 158
Rep Power: 15 |
hi Mahzad
I browsed a lot to find experimental or numerical results in very low reynolds number, but unfortunately, I ve never found it. In fact this Re range is rarely simulated, I don't know why. however, I have some experimental or numerical results that is higher than the range that you want. if it is useful for you, please send me an e-mail to send them to you. but if you develop a code, I recommend you to validate your code with result of a software such as Fluent. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
literature data for simulation coal combustion | darookie | CFX | 1 | April 29, 2014 09:50 |
Interpolation of data on interfaces during initialization | Chander | CFX | 7 | August 16, 2011 13:15 |
Exporting transient simulation data for evey time step | mali28 | FLUENT | 1 | August 3, 2011 12:48 |
Simulation of transonic flow over NACA0012 airfoil | MSc Student | Siemens | 2 | August 9, 2006 14:49 |
Ventilation Simulation & Experiment Data | Luo Shengping | FLUENT | 2 | November 30, 2000 05:00 |