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
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
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
>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
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
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