![]() |
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 |
#35
|
|||
|
|||
![]()
Jon Meyer wrote in message ...
Bernhard's diagrams are spot on, but whether you call it thrust or a reduction in drag is up to you. My Aeronautical Engineering textbook uses both as alternative ways of describing it. It all depends on how you choose your frame of reference. The winglet produces a vorce vector which consists of drag and lift, but when this force vector is considered with the sailplane as the frame of reference then its components could be considered as a thrust force and a lateral force. I feel that this is the easier way to describe the way they reduce overall drag, but if you want to be pedantic........ If there is only drag and no thrust you'll eventually be flying backwards, right? Suppose you raise your glider up into the air under a balloon and drop it. If the wings (nor anything else) generate only lift and no thrust then you'll just move in the verticle direction only, or hover. If a wing can generate thrust then so can a winglet depending on geometry, AOA etc. It will also generate drag and weight. -- FF |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
A Level 1 AOA clarification | Ramapriya | Piloting | 64 | January 9th 05 01:19 AM |
Space Elevator | Big John | Home Built | 111 | July 21st 04 04:31 PM |
max altitude and Mach 1 | Boomer | Military Aviation | 22 | June 1st 04 08:04 PM |
Proposals for air breathing hypersonic craft. I | Robert Clark | Military Aviation | 2 | May 26th 04 06:42 PM |
P-38 Exhaust | Stephen Harding | Military Aviation | 10 | April 19th 04 07:03 AM |