![]() |
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 |
#7
|
|||
|
|||
![]()
I'll need to find a site. Sounds interesting. Thanks.
"Paul Lee" wrote in message om... Have you looked at those vortex generator tabs placed on top of the wing. Very negligible top end decrease. They come in a kit and are easy to apply. Users claim 5-10 kt decrease in stall. "Dick" wrote in message om... Just for discussion, what opinions are there for an individual lowering the stall speed of an existing wing considering constructability and cost? I remember there was some leading edge profile modification studies done years ago but can't see that as a practical approach for an individual. Thinking about how to add sailplane-type upper surface spoilers, WW2 fighters underwing dive brakes, etc. Dick |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
Canard planes swept wing outer VG's? | Paul Lee | Home Built | 8 | January 4th 04 08:10 PM |
Calculating vertical time and distance in a stall turn (US Hammerhead) | Dave | Aerobatics | 3 | November 20th 03 10:48 AM |
Wing Extensions | Jay | Home Built | 22 | July 27th 03 12:23 PM |