Jan 25, 2017 #1 tomo pauk Creator of Interesting Threads 13,878 4,399 Apr 3, 2008 The data on the S-3 wing profile, as used eg. on P-47 or P-43 seems elusive. Though one web site states it have had a 11% thickness-to-chord ratio at 30% of span. Any data around?
The data on the S-3 wing profile, as used eg. on P-47 or P-43 seems elusive. Though one web site states it have had a 11% thickness-to-chord ratio at 30% of span. Any data around?
Jan 25, 2017 #2 GrauGeist Generalfeldmarschall zur Luftschiff Abteilung 27,946 21,966 Aug 29, 2008 Redding, California www.netallurgy.com Tomo, have a look at this airfoil data: REPUBLIC S-3 AIRFOIL (s3-il)
Jan 25, 2017 Thread starter #3 tomo pauk Creator of Interesting Threads 13,878 4,399 Apr 3, 2008 Thanks, Dave - that is exactly the web page I was making a hint above. Unfortuantely, I'm unable to find the T-t-C ratio at root and at tip.
Thanks, Dave - that is exactly the web page I was making a hint above. Unfortuantely, I'm unable to find the T-t-C ratio at root and at tip.