![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#1
|
|||
|
|||
![]()
I have the copy of the CAFE test of Cozy Mk IV canard where it states
that swept wings tend to start stalling at the tip rather than the root. This moves the center of lift forward and is a bigger problem for aft CG. While canard planes swept wings typically already have those "vortilon" tabs, has anyone investigated placing a few vortilons near outer wing part to compensate for the early tip stall tendency? I am talking about the main swept wing of a typical canard and not the front canard wing itself. ---------------------------------------------------- Paul Lee, SQ2000 canard project: www.abri.com/sq2000 |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Proposed new flightseeing rule | C J Campbell | Home Built | 56 | November 10th 03 05:40 PM |
wing root strakes (not canard A/C) | Wallace Berry | Home Built | 0 | October 2nd 03 08:47 PM |
Props and Wing Warping... was soaring vs. flaping | Wright1902Glider | Home Built | 0 | September 29th 03 03:40 PM |
Can someone explain wing loading? | Frederick Wilson | Home Built | 4 | September 10th 03 02:33 AM |
Wing Extensions | Jay | Home Built | 22 | July 27th 03 12:23 PM |