![]() |
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
|
|||
|
|||
![]() kd5sak wrote: "Richard Lamb" wrote in message nk.net... TRUTH wrote: "Jim Macklin" wrote in news:uX8Lf.104268$4l5.39451@dukeread05: Bernoulli theory: So how do these equations relate to our two-dimensional airfoil? Look again at the Clark Y and notice that an airfoil is a curved shape. While the bottom is relatively flat, the top surface is thicker and more curved. Thus, when air passes over an airfoil, that flow over the top is squeezed into a smaller area than that airflow passing the lower surface. The Continuity equation tells us that a flow squeezed into a smaller area must go faster, and the Bernoulli equation tells us that when a flow moves faster, it creates a lower pressure. I don't quite understand the "squeezed into a smaller area". I Understood that the flow over the top surface had to travel further (thus faster) over the longer curved distance to get from the leading edge to the back of the airfoil. I am just a lay person and do not even play an aeronautical engineer on TV so I may be totally mistaken. You are, but don't feel bad. It is a common misconception even still taught by some flight instructors. The truth is, there is nothing connecting molecules of air together. It does not matter that a molecule above the wing has to travel farther in order to 'catch up' to one below the wing. It never met the lower molecule and cares nothing about it. :-) Airplane wings use the curved upper surface to displace air which, because it is slightly sticky, follows the surface of the wing. If you hold a water glass sideways under a stream of water you will see the water curve around the glass all the way to the bottom. Air flowing over a wing does the same thing. As you probably learned in basic physics, though, gases like air maintain a constant total pressure. Air is being accelerated in one direction over the wing, so pressure is being increased in a single direction. We call this dynamic pressure. It is the pressure you feel when you blow on your hand. If dynamic pressure in one direction is increased and total pressure must remain constant, then the pressure in all other directions must be decreased. We call the molecules moving in all these other directions the static pressure. It is like cars in a parking lot, all moving in different directions. If most of them reach a road and start moving in a single direction, then there must be fewer cars moving in other directions. Since most of the air particles are being accelerated in a single direction then there must be fewer of them moving in any other direction. This creates an area of low pressure above the wing. Air above the wing moves into this low pressure area and is in turn accelerated behind and down off the trailing edge of the wing. Newtonian physics tell us that if there is acceleration in one direction there must be an equal and opposite reaction in the other. We call that lift. The amount of lift generated is computed by an equation involving the air density, speed of the wing, area of the wing, and something called the lift coefficient which is basically how much air can be displaced by the wing. Thus, wings generate lift by accelerating air over the top of the wing and then down off the trailing edge. People don't realize it does this because they see pictures of air streams taken in wind tunnels, where the fan continues to blow the air straight backward behind the wing. In actual flight, however, the wing is simply forcing a huge volume of air straight down. You can see this when an airplane flies low over water; the ripples in the water are almost directly below the airplane. Really, a wing is just a big fan blade, only instead of spinning around it moves in a straight line. You do not stand at the edge of the fan to catch the breeze it generates. You stand behind it. You also know that the air blown by a fan comes from in front of the fan. You can hold strips of paper in front of a fan and watch them being sucked toward the fan. Well, the wing is just a fan blade. A great big fan blade, to be sure, but that is all that it is. We call it Bernoulli's principle because Bernoulli was the first to notice that if you accelerate a fluid in one direction that pressure in the other directions is reduced. One method of accelerating a fluid is to force it through a tube that narrows, which is what Bernoulli did. Wings do not really do that, although you commonly see science popularizers showing air flowing through a Bernoulli tube and then removing half the tube and calling it a wing. The fact is, air is not really being compressed in that way at all. It is simply being accelerated over the top of the wing by the front part of the curved surface. That is why lift is greatest at the point where the wing is thickest. Nevertheless, Bernoulli's equations work well for predicting lift even though the method of accelerating the air is slightly different than forcing it through a narrow tube. It is the same principle, just differently implemented. The Wright Brothers actually found that wings generate somewhat more lift than would have been first predicted by Bernoulli. Their first wings were too thick with a greatly exaggerated curve in order to generate maximum lift. What they discovered through trial and error, though, was that although such a wing generated a great deal of lift it also could not generate more by increasing the angle of attack -- the angle with which it meets the air. Instead, what they got by increasing angle of attack was complete separation of air flow from the wing and lift went to 0, what we call a stall. This is one reason the Wrights never rebuilt the first Flyer after it was destroyed shortly after making its first flights. They realized that the machine would never be able to climb very rapidly and that it would always be prone to suddenly falling out of the sky because of stalls. They considered the thing to be extremely dangerous and went back to the drawing board. Also, of course, they destroyed it to keep it out of the hands of potential competitors like Curtis. A shame, really. Or, you can just take the simple explanation and say that the air has to travel further over the wing in order to generate lift. It is wrong, but it works well enough for laymen. |
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 |
GAO: Electronic Warfa Comprehensive Strategy Needed for Suppressing Enemy | Mike | Naval Aviation | 0 | December 27th 05 06:23 PM |
Washington DC airspace closing for good? | tony roberts | Piloting | 153 | August 11th 05 12:56 AM |
Sport Pilot pilots not insurable? | Blueskies | Piloting | 14 | July 12th 05 05:45 AM |
USAF = US Amphetamine Fools | RT | Military Aviation | 104 | September 25th 03 03:17 PM |