![]() |
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
|
|||
|
|||
![]()
At 04:59 28 February 2015, Paul Villinski wrote:
As a non-scientist/engineer, it baffles me that we are able to build amazin= gly sophisticated airplanes, yet, as the lecturer demonstrates, there is a = huge amount of confusion over how to explain why a wing produces lift, and = many of our common assumptions are simply wrong, i.e., the reason(s) for ac= celerated airflow over the top surface (which intuitively has never made se= nse to me). Engineers designing airplanes are themselves still arguing over= whether it's more about Bernoulli or the downward-turning force or Coanda = effect. Yet, I'm still able to get from one coast to another at 35,000 feet= traveling at 600 mph, while sipping coffee and watching a movie. A reasonable parallel is the dual nature of light, which can be treated as both wave and particle. Both models explain the result. John Firth |
#2
|
|||
|
|||
![]()
Glider wings work on faith.
It's easy to have faith at 4-5000ft so the wings work well & soaring is easy. 'Tis more difficult to have faith at 1000ft so wings work less well & gliding is more tricky. Much below 1000ft I lose all faith & land shortly after. This assumes UK feet where 5000 is "High" not American / Australian / South African feet where 5000 is "Low". KN At 15:36 28 February 2015, John Firth wrote: At 04:59 28 February 2015, Paul Villinski wrote: As a non-scientist/engineer, it baffles me that we are able to build amazin= gly sophisticated airplanes, yet, as the lecturer demonstrates, there i a = huge amount of confusion over how to explain why a wing produces lift and = many of our common assumptions are simply wrong, i.e., the reason(s) for ac= celerated airflow over the top surface (which intuitively has never made se= nse to me). Engineers designing airplanes are themselves still arguing over= whether it's more about Bernoulli or the downward-turning force o Coanda = effect. Yet, I'm still able to get from one coast to another at 35,000 feet= traveling at 600 mph, while sipping coffee and watching a movie. A reasonable parallel is the dual nature of light, which can be treated a both wave and particle. Both models explain the result. John Firth |
#3
|
|||
|
|||
![]()
The biggest problem is trying to prove up the % saved. Then you have to convince the bean counters.
![]() Quote:
|
#4
|
|||
|
|||
![]()
I must admit that I didn't read the article thoroughly, but it seemed to
me by looking at the picture that the thing would enhance wingtip vortices (the Windows spell checker did not like that word, BTW). Anyway, I thought the idea was to reduce vortices since they're wasted energy that could be used by the aircraft. Aero engineers, please chime in. On 2/28/2015 2:54 AM, Skypilot wrote: The biggest problem is trying to prove up the % saved. Then you have to convince the bean counters. ![]() ND;897867 Wrote: interesting article about a potential winglet replacement for jets. I personally think that winglets have more sex appeal though, especially maughmer's. http://tinyurl.com/37q5aeb -- Dan Marotta |
#5
|
|||
|
|||
![]()
On 2/28/2015 10:19 AM, Dan Marotta wrote:
I must admit that I didn't read the article thoroughly, but it seemed to me by looking at the picture that the thing would enhance wingtip vortices (the Windows spell checker did not like that word, BTW). Anyway, I thought the idea was to reduce vortices since they're wasted energy that could be used by the aircraft. Aero engineers, please chime in. I had the same off-the-cuff gut reaction when I first looked at it, too. Upon further cogitation, I'm still uncertain eggzackly what-n-how the designer was seeking to achieve what I think he was seeking to achieve. I also noticed the article said he was an aeronautics teacher, so this may be a case of: Those who can't do, teach! In any event, I'm not investing my retirement in any company trying to make and sell these babies... Bob W. |
#6
|
|||
|
|||
![]()
On Sat, 28 Feb 2015 16:54:40 -0700, BobW wrote:
On 2/28/2015 10:19 AM, Dan Marotta wrote: I must admit that I didn't read the article thoroughly, but it seemed to me by looking at the picture that the thing would enhance wingtip vortices (the Windows spell checker did not like that word, BTW). Anyway, I thought the idea was to reduce vortices since they're wasted energy that could be used by the aircraft. Aero engineers, please chime in. I had the same off-the-cuff gut reaction when I first looked at it, too. Upon further cogitation, I'm still uncertain eggzackly what-n-how the designer was seeking to achieve what I think he was seeking to achieve. I also noticed the article said he was an aeronautics teacher, so this may be a case of: Those who can't do, teach! In any event, I'm not investing my retirement in any company trying to make and sell these babies... Bob W. I had good results with a form of Hoerner tip on my F1A competition models (wings 2011mn span, 150mm parallel chord centre panels, short tips tapering to 100mm chord by keeping the TE straight and sweeping the LE back. The general tip design guidelines I used we - sweep the LE at least 10 degrees to promotee spanwise flow on the top surface - rake the edge of the tip about 30 degrees with a smooth, rounded join to the LE and a sharp, acute angle join to the TE - the tip's outside edge should follow the lower surface of the airfoil with the upper surface smoothly blended down to meet the lower surface at an acute angle. The idea was for the spanwise flow to help move the tip vortex out from the tip while the pointed TE would help stability by localising the tip vortex. My wings had carbon D-boxes with open structure behind that. The tips themselves were carved from block balsa, finish sanded and covered with a doped-on layer of 25 gsm glass-cloth. It all worked pretty much as I hoped. The design flew well enough to be competitive and was extremely stable and well-behaved in all sorts of air. There was an unexpected bonus too: the glass covered tips were very tough. I lost count of the number of times those models got overturned after landing and blown down blacktop runways upside down, but always with remarkably little damage to the tip blocks. -- martin@ | Martin Gregorie gregorie. | Essex, UK org | |
|
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
A wingtip | Glenn[_2_] | Aviation Photos | 5 | September 3rd 10 03:33 PM |
Yet another PA-28 wingtip query... | Mike Spera | Owning | 2 | August 4th 09 03:07 AM |
Wingtip Camera | NG[_2_] | Soaring | 14 | April 9th 09 11:38 PM |
Wingtip Camera | kestrel19 | Soaring | 0 | April 9th 09 04:02 PM |
L-23 wingtip wheel modification | 5Z | Soaring | 0 | February 8th 06 05:50 PM |