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Damaged tops
Most of the tops of the containers i saw at FIRST were cracked and some of ours are as well..........so dont count on sucking on the top of the container .......it really sucks.
Jim:rolleyes: |
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All planes change their AOA (angle of attack) not just modern planes. To climb a plane lowers it's tail and points up, increasing the angle of attack and gaining more lift. Greg |
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The other way is to push down on a suction cup until it's flat. Push down on the cup with a ring and then pull up on the center. How hard a vacuum you get depends on how hard you pull. But there isn't much volume so a slight leak could be trouble. |
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While we are all aware of the *top secret* "Magic Smoke" factories that produce that crucial component installed in every electrical and electronic device; few people are aware of the small "Homesick Angel" installed in every type of aircraft.
Unfortunately (for aircraft designers) they have no say in which angel they get and some are more "homesick" than others. Early attempts a flight were often thwarted by the fact that most of the angels found here on earth were in no hurry to get back home. However, as time has passed and more and more aircraft take to the skies, more angels have been lured to earth. By the way - I'd consider this thread officially *Hi-Jacked* <G> |
Suction Cups How
Why can't you hook your suction cups up to the intake of the compressor. It is on the left side when looking at the motor end. It has the white felt filter. Does anyone see how this would violate the rules????
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Seems like the only way to create a vacuum is to have a motor (or another cylinder) pull a cylinder. |
how to vaccum
You can't use the venturi effect to create a vaccum. What we might do is have to opposing pistons, one using the compressed air to have the other piston create a vaccum.
As for the airplane debate, I think it's the bernoulli effect. Or at least that's the most important component. The angle of attack does make a difference though but it's important with the wing shape, that's what the Wright brothers figured out. The curvature of the surface of the wing has low pressure, the bottom end has high pressure. Since you've got a plane with wings that have a large surface area, you've got a lot of lift force overall. The important part to lift is airspeed. If planes relied entirely on angle of attack, then in theory, your flaps that angle down would make the plane lift up on landing. (not too sure about that) |
Suction Cups How
Wll when I took the compressor apart it looks like the only place air comes in is from the white felt area. Port A is discharge and B is the relief. Air should not normally come out of B. Some how you would have to hook an air sitting up to the white felt area but then this might be constued as altering the compressor.
So what we are going to do is use the fisher price motor to pull a cylinder to create vacumn. If you look at the threaded rod that came with the kit it appears as if it and the black plastic nut were designed to fit with the fisher price motor gear box. It sucks that you just can't use an eductor. |
Wing Lift
I had to jump in on this one - sorry.
The equation for the lift generated by an airfoil is: Lift = 0.5 * CL * (AirDensity) * (Wing Area) * V^2 Where CL is the coefficient of lift and V is the airspeed over the airfoil. From the above formula it is obvious that as airspeed increases lift also increases. What is not obvious is how CL is determined. CL is a function of the wing shape AND the angle of attack. For actual airfoils, CL is determined experimentally in a wind tunnel for all angles of attack (i.e. they make a CL vs. angle of attack graph). For thin airfoils and small angles of attack, you can approximate CL with the following formula: CL = 2*pi*(Angle of Attack) [angle of attack must be in radians] How exactly is lift created? That is a debate that will go on forever. It is partially Bernoulli effect and partially Newton's 2nd Law - how much of each is subject to debate. Actually, some aerodynamicists have suggested that in the case of an airfoil, one principal can be used to explain the other. In all honesty, it's not really all that important as long as lift can be calculated accurately. Someone made a statement about flaps. Flaps are used to increase the angle of attack of the airfoil and change its camber (shape). This is done so that the airplane can get larger amounts of lift at slower airspeeds and lower deck angles (like what is required during landing). By changing the wing camber, flaps also increase the stall speed of the airplane (which is also good for landings since it allows the plane to land at a slower speed). Flaps also add a lot of drag which allows the plane to make a steeper approach without having to do a forward slip (which are fun for the pilot but they tend to freak out the passengers). -Chris |
dual-cylinder vaccuum device
We created a setup of two cylinders attached together by their threads and bolted it to a piece of lexan. the only problem is when you create a vacuum the lexan sheet will bend. we'll probably use aluminum instead. the suction cups we have work great on the sides of the boxes, but they are horrible on the top of the box, mostly because the tops crack too easily and the texture is diiferent on the top than on the bottom.
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