KR> CL eqns available ?? Stall speeds

2008-10-12 Thread Mark Langford
Wesley Scott wrote: > Did Ashok publish an equation or a set of tabular data for the wind tunnel > results? I hate trying to read data off of graphs. (See > http://www.krnet.org/as504x/repeat_1m.gif ). If it's not published at http://www.krnet.org/as504x , you're probably not going to find it

KR> CL eqns available ?? Stall speeds

2008-10-12 Thread Wesley Scott
Did Ashok publish an equation or a set of tabular data for the wind tunnel results? I hate trying to read data off of graphs. (See http://www.krnet.org/as504x/repeat_1m.gif ) Looking at the graph it appears the best CL to operate at is approx 0.72. The point where Cd starts to increase with incr

KR> CL eqns available ?? Stall speeds

2008-10-12 Thread Wesley Scott
It wasn't readable so this time I pasted into notepad to convert it to plain text and then still had to add formatting. It should be in straight ascii now. The numbers are based on the CL values of the AS5045 airfoil taken from the graph http://www.krnet.org/as504x/repeat_1m.gif The predicted bes

KR> CL eqns available ?? Stall speeds

2008-10-12 Thread larry flesner
>It wasn't readable so this time I pasted into notepad to convert it to plain >text and then still had to add formatting. It should be in straight ascii >now. Wes, I'm still having trouble making sense of the numbers. My KR at approx 1075

KR> CL eqns available ?? Stall speeds

2008-10-12 Thread Wesley Scott
t and velocity. I'll try to describe it after getting some sleep. -- wesley scott k...@spottedowl.biz - Original Message - From: "larry flesner" To: "KRnet" Sent: Tuesday, July 06, 2004 6:30 PM Subject: KR> CL eqns available ?? Stall speeds > > >