RCU Forums - View Single Post - Spanwise Lift and Stall Sequence
View Single Post
Old 02-25-2010 | 04:49 PM
  #18  
da Rock
Senior Member
 
Joined: Oct 2005
Posts: 11,517
Likes: 0
Received 2 Likes on 2 Posts
From: Near Pfafftown NC
Default RE: Spanwise Lift and Stall Sequence


ORIGINAL: victorzamora

Mechanical twist is LITERALLY twisting the wing to LITERALLY vary the angle of attack of the wing along the semispan.

I don't think that elliptical wings stall at the TE of the root first, and the picture showing stall tendencies shows that.

I'm betting you'd rather say that "Mechanical twist actually twists the wing from root to tip to actually vary the angle of attack of the wing along that semispan."

Also, if you look closely at the elliptical wing and compare it to the rectangular one, you'll see that the rectangular one definitely shows the stall originating at the TE at the root of each halfspan. Compare the arrows that show how the stall migrates out from one specific location, the TE @ the root, to the similar function arrows showing the migration of the stall on the elliptical planform. That elliptical stall's arrows come from along a significantly wide span of the wing's TE. You are correct, elliptical wings do not stall at the root TE, however the picture doesn't show that happening.