View Full Version : Twist in Bell 205/UH-1 Blades ?
Hueyman
23rd Jan 2016, 17:41
Hi Gents,
Does anyone know the twist in degrees of the Huey rotor blades, from root to tip ?
Simple info but can't find it anywhere.
Thank you !
Hueyman
It's 10 degs on a 206, so probably roughly that.
phil
Gordy
23rd Jan 2016, 20:04
It is -11:
http://i76.photobucket.com/albums/j35/helokat/Huey%20205/blade_zpsycsog6na.jpg
Hueyman
23rd Jan 2016, 22:08
Hi,
Thank you very much for your reply, much much appreciated !
Do you know where I could have good reads or topics on that particular teetering rotor system, how it aerodynamically works, what to k,now about the stabilizer bar dampeners, pre-cone angle purpose, drag brace degree of freedoms etc... everything related to that head design ?
Thank you again,
Hueyman
axelrush
1st Mar 2022, 01:58
Hello there!
Does anyone know the twist in degrees of the Bell UH-1 rotor blades?
Thank you !
Ascend Charlie
1st Mar 2022, 05:34
I think it was a total of 10 degrees, something like +7 at the hub and -3 at the tip? But the brain is old...
11 on the 212 if it helps
axelrush
2nd Mar 2022, 07:32
I ll take that as correct, thanks a lot dude! Greetings!