CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums

Entries for May 15, 2014

Register Blogs Community New Posts Updated Threads Search

Old

TSAGI HERITAGE, NACA23012, M=0.5, alpha = -1.2 grad

Posted May 15, 2014 at 03:09 by skeptik (CFD notes)
I have some useful papers totally on Russian.

I will post some experimental results about airfoils here as i will translate it to appliciable form.

Here are the results which could be easily plotted by GNUplot. They are from far away 1946, TSAGI (Central Aero-, Gas-Dynamics Institute) publisher.

Code:
#NACA 23012 exp. results alpha = -1°12' M=0.5
# Cp=(Pfoil - Pinfinity)/q; q = rho*U^2/2
#columns
#    x, %    Cp
#Upper
1    0.6
...
Continue reading...
Attached Thumbnails
Click image for larger version Name: output1.png Views: 781 Size: 7.6 KB ID: 223  
Member
Posted in Uncategorized
Views 1139 Comments 0 skeptik is offline Edit Tags

All times are GMT -4. The time now is 01:12.

Contact Us - CFD Online - Privacy Statement - Top