I took this off SSW because I thought it was a good question, one I surely can't answer. I do know I get really good performance with APC narrow blade props though, I just have no idea why. This is not my question, but I'm interested in the answer.
Quote:
"Recently I started using some of the Top Flite Power Point props, they work pretty well,(and they are available at the local hobby shop), they have narrow bldes as compared to the old Rev-ups or even the Zinger props. Does anyone have an opinion what might be better, wider blades, or the thinner type such as the Top Flite variety? Any reasons why one might be better than the other?"
I've looked for this sort of information on the web, and boy is it scanty! Wikipedia does have a good entry, if you look for their article on airplane propellers:
http://en.wikipedia.org/wiki/Propeller_%28aircraft%29. It's scanty, but it seems to be on target with what's there.
I suspect that this is because the question "what makes a prop do what a prop does" doesn't have a really simple answer. From what I can gather, from the general aerodynamics books that I have and from readings on the web, this is something that could consume years of your time in a University course of study; anything that we do as modelers is going to be vastly oversimplified. One of these days I want to find a book that goes into it, but I expect that if I do I'm going to regret the fact that I'm an electrical engineer, not a fluid dynamicist.
Here's what I know, and it's all vague and confusing:
A prop is just like a wing, only it's spinning.
A prop is just like a wing:
This means that anything rule that you can apply to a wing -- area, aspect ratio, angle of attack, etc., all apply to props. I've even seen props on full-size airplanes with sorta-Horner 'wing' tips (on a Piper Cheyenne III owned by the US Customs Service). This also means that airfoil choice is important, as is surface finish and the lift distribution over the diameter.
Just from momentum vs. energy considerations, a big slow prop is going to use less power to generate a certain amount of static thrust than a little fast prop. Ditto big & two-blade vs. little & three blade, or big & low pitch vs. little & high pitch. It's just like a glider vs. a fighter jet. Consider a helicopter main rotor -- in a way, it's just a propeller. But it needs to generate lots of lift at really low airspeeds (think "hover") -- so compared to a propeller that you might use on a same-sized airplane, it's got really skinny blades, it's really big, and it's really slow. On the other hand, take the motor out of the helicopter and put it on a racing plane, and all of a sudden you want a little, high-pitch prop.
There are obvious issues with really skinny blades -- how in heck are they going to hold together? Also, as speed goes up the induced drag (that which comes from diameter vs. thrust) claims a smaller and smaller proportion of the total drag than parasitic drag (that which comes from pushing all that material through the air).
Only it's spinning:
Because the prop is spinning, its potential for generating lift changes from the root to the tip. Worse, even at a constant RPM the distribution of lift from root to tip will change with airspeed -- and an efficient prop at low airspeeds isn't efficient at high airspeeds, and visa-versa. Worse yet, the "pitch" (the amount of lead built into it, as if it were a bit of screw thread) can and should vary over the diameter of the blade -- and each manufacturer is going to have a different idea of what this variation should be.
None of this helps to answer your question -- if I've done anything good with this babbling, it will only serve to give you more specific questions to ask. There are so many variables to this that I don't think a universal ideal will ever be found. I think the "ideal" stunt propeller is going to be one that is matched not just to the airframe and engine, but to the flying style of the pilot. I think that the elements that go into making the prop 'best' are going to go beyond mere aerodynamics -- at the very least they're going to extend to structural integrity, weight (and gyroscopic properties), and maybe even aesthetics (what if the prop that flies the best has a butt-ugly shape -- would you use it?)
So, should someone out there start working up a report on propellers, I think that these are the points you should think about:
* What is its aspect ratio (i.e. blade area vs. diameter)?
* What is its pitch distribution (i.e. blade angle vs. diameter)?
* What is the area distribution (i.e. blade width vs. diameter)?
* What is the airfoil? Does it change with diameter?
* What is its surface finish?
* Does it curve (i.e. is it a scimitar prop)?
* How does it fly a big light slow plane?
* How does it fly a little heavy fast plane?
* How do a half a dozen of your buddies like it, in each of the above planes? Why?
* How does it pull on the flat?
* How does it pull up a vertical?
* How does it behave down a vertical?
* How does it seem to affect inside corners?
* How does it seem to affect outside corners?
* How does it accelerate out of a corner?
When you're all done, things will still be incredibly vague -- but if we're all lucky we'll at least have some general guidelines!
I would do this report, but for two things: (1), I wouldn't get it done until I'm 102 years old, and (2), the most likely report for any props I test would be "broke on flight number (1 through 4) when I crashed".