![]() |
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 |
#11
|
|||
|
|||
![]()
"Steve House"
wrote: According to my textbooks that's not true. Maximum lift is just before the stall. Once in the stalled condition itself, at or beyond the separation point of the flow of air over the airfoil, lift is lost and "the airplane ceases to fly." (From The Ground Up, Aviation Publishers, Ottawa, page 35 and Flight Training Manual, Transport Canada, page 75) You completely misunderstand stall and your misunderstanding is perpetuated by the complained-about programming. Maximum lift is just before stall and just after stall the lift is just about equal to that maximum. Understanding that lift is produced during stall is essential to a proper understanding of spins and aerobatic flight. Of course not all lift is gone - if you want to get picky about it, even a dropped brick has SOME lift - The lift remaining just after stall is almost the same as the lift just prior to stall, and is still supporting almost all of the aircraft's weight. but what does remain is insufficient to support the weight of the airplane The one difference is that as AOA increases, lift decreases, and since the aircraft is designed to increase AOA when the wings are not producing enough lift, after stall, the plane automatically produces less and less lift if the pilot allows the pla ne to "do its thing" and increase AOA further. It is actually possible in some fully aerobatic high-powered aircraft to supplement the small amount of missing lift from a stalled wing with engine thrust. The plane can then be flown with the wings fully stalled. I saw it demonstrated last year. Similarly, some spin modes have both wings fully stalled, and the descent rate is constant. Thus, the wings are fully supporting the weight of the aircraft with the lift produced when stalled. and as you said in another message, the airplane is indeed falling rather than flying. Thus "at the stall" would be the point at which the wing stops producing (adequate) lift, just as he said. Saying it produces less lift after stall is correct. Saying it stops producing lift is not correct and is highly misleading. Todd Pattist (Remove DONTSPAMME from address to email reply.) ___ Make a commitment to learn something from every flight. Share what you learn. |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Is this the end of Discovery Wings Channel ?? | LJ611 | Home Built | 16 | December 7th 04 04:26 AM |
Discovery Wings Channel ??? | Jerry J. Wass | Aerobatics | 3 | November 15th 04 03:31 PM |
Discovery Wings Channel ??? | Andy Asberry | Home Built | 0 | November 13th 04 05:11 AM |
Discovery Wings Channel ??? | RobertR237 | Home Built | 1 | November 8th 04 08:40 PM |
Disc. Wings Channel | Darren Eccles | Instrument Flight Rules | 6 | December 24th 03 08:08 PM |