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lr32
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golf balling
from lr32
wrote 3 years 15 weeks ago
The dimples are for preventing separation by inducing a turbulent boundary layer. Most aircraft have turbulent flow over most of their surfaces anyway, partly because the Reynolds number is far higher, which means that, since they're larger and faster, viscosity is less important. You CAN have a lot of laminar flow instead of turbulent if all your aircraft's surfaces are very smooth and well shaped, but most metal aircraft don't meet this standard. If I'm not mistaken, at higher Reynolds numbers, even laminar flow is less prone to separation.
Still, you do see a line of bumps on some sailplane wings, fairly far back. Also, there are vortex generators on light aircraft (and others) which I don't think are entirely the same, but which stir up the boundary layer to prevent separation. I think in this case with vortices.
The Buick probably had lots of separated flow where there were sharp corners or sudden reductions in cross section. Still, 15 percent seems like a lot.
Perhaps a Cessna Skymaster with the rear engine out would benefit from dimples. With the rear engine on it helps keep the flow attached.
Until the advent of better airfoils, we would often use "turbulators" on model aircraft to improve performance. A turbulator is a discontinuity which would accomplish much the same thing as those dimples. Probably with less drag because it's only in one spot instead of all over.
nifty image of more and less separation here:
http://www.efluids.com/efluids/gallery/gallery_pages/wake_page.jsp
With attached flow, you get pressure recovery (i.e. more pressure) on aft facing surfaces, and so less drag.
I'm not a fancy aerodynamicist and I can't do all the math (although I can do some of the simpler stuff), so don't take my word as gospel.
Flat paint
from lr32
wrote 3 years 15 weeks ago
It's my understanding that if it's SMOOTH flat paint, it doesn't hurt you, even on a "laminar" wing. And there may be an advantage that in the rain the water doesn't bead up the same way. OTOH, I bet waxed paint is more durable and easier to remove bugs from.
I'll bet if you used sandable primer, patience, and a long sanding block, you could increase the extent of laminar flow, whether you were using gloss paint or not. But how much difference that makes on an RV, or how durable your paint job would be, I don't know. The sailplane guys sometimes do some sanding and rework to get more perfect, non-wavy shapes.
Avoid paint lines ahead of transition from laminar to turbulent flow. Aft of that, it doesn't matter much.
From everything I've read, it might be more worthwhile for you to look closely at cooling drag and lots of little intersections, air leaks, and details on your plane.
caveat: I'm a model airplane guy and not an aerodynamicist, though I am an engineer.
Pushers, Canards and Diesel Rotary Engines - why?
from lr32
wrote 3 years 15 weeks ago
I don't know about inside, but outside the plane pushers are usually noisier, and they tend to sound really weird. I think that's because they are operating in disturbed flow which isn't the same all the way around.
I seem to recall Peter Garrison covered the topic of pusher props vs. conventional in a recent column. On a push me pull you aircraft like the Cessna Skymaster, that rear prop can keep flow attached over more abrupt transitions. I seem to recall that in the column, it seemed that which one was better depended to a large extent on the details of the individual aircraft. If you could get symmetrical flow into the pusher prop, and a modified prop design, it would probably be a lot more efficient. But that doesn't usually happen. There are some neat articles on the CAFE web site of how much drag you can get rid of with axisymmetric fuselages with axisymmetric flow and a pusher prop. So just get rid of your wings. Might make sense for a dirigible or submarine.
A tractor prop is going to increase airspeed over the fuselage, and, as I recall, is supposed to create bands of turbulent flow, though I understand that on something like the Nemesis, the flow is laminar in between those bands.
My understanding is that the Long Eze, or perhaps it was the Varieze, was wind tunnel tested, and the prop was very innefficient, but the rest of the airframe was very low drag.
The Piaggo Avanti, a pusher, is supposed to be efficient, but it sure sounds loud and weird.
Canards, like many other configurations, can be quite stable. However, on a stable aircraft the rear surface must be more lightly loaded than the front. So you probably need more wing area to support a given weight, and the canard has to work very hard.
An alternative is the three surface airplane such as the Piaggo Avanti. This can have, I recall reading, lower trim drag than some others. Or at least the induced part of the trim drag can be lower. If it's done right.
I think wankels would show up on airplanes a lot more often if they were on all our cars and we'd been developing them for 100 years.
Technicalities: efficiency of canards over tractors
from lr32
wrote 3 years 15 weeks ago
For stable flight, the aft surface needs to be more lightly loaded. If you make it large, you need lots of extra wing area that is just loafing. Meanwhile, the canard has to lift really hard. So, all else being equal, which it never is, you could make a conventional configuration with less area, or the same area with a lower stall speed.
The tail on a conventional configuration isn't always pushing down. Perhaps on a particular Cessna, I suppose. However, if the tail is big enough and far enough back, and the cg is far aft enough, the horizontal stab could be pushing up. In any case, the load is probably small.
This isn't just theory. I've built EZB's, which are a very, very light indoor model airplane, where the tailboom bends up a little bit in flight. Sometimes the c.g. is behind the trailing edge of the wing. Of course the tail is 50 percent of the area of the wing, so that's an extreme case.
Note that nearly all sailplanes, which MUST be efficient, have the conventional configuration. That's not an accident.
Electric power
from lr32
wrote 3 years 15 weeks ago
Greener than using a piston combustion engine. It is my understanding that large scale electrical generation is far more efficient than a small piston engine operating at part throttle. Of course, some of this depends on how heavy the batteries are.
Can't argue about battery disposal except I wonder if lithium batteries are nearly as toxic as nicads, lead acid, etc. which are NOT going to show up as batteries to power aircraft motors. Probably the batteries are well worth recycling in any case.
I think the gas is just hydrogen. A fire hazard but I bet not an environmental one.
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