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Quote:
![]() To compare data, it should be with a lip and an open exhaust on the bench I think. I`m using the two tube ET airspeed sensor. I don`t know what other meathods are available, but I`m just looking for any data that I can find at this point. |
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Latest blog entry: EDF, My First Six Years, mostly Pictures
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I'm pretty sure it was open exhaust, but I'd have to go back and read his text.
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Latest blog entry: EDF, My First Six Years, mostly Pictures
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Lee,
It is interesting to note that fan manufacturers market high pitch, lower blade count fans for the highest performance. For scale sound it seems they go with higher blade counts and less pitch. For the speed: http://www.stumaxaircraft.com/pages/SM110-45.htm http://www.schuebeler-jets.de/en/hdt...4-dia-hdt.html |
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This chart seems to verify that and if you look at efflux speeds posted for Dynamax you'll see speeds approaching 300 also. The key is how much power a given rotor can handle before it blows up. |
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Latest blog entry: EDF, My First Six Years, mostly Pictures
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Lee,
If these charts you're referring to are the result of static testing one could argue that a high blade count fan has an advantage accelerating static air. A higher pitched, low blade count rotor might not perform as well statically but you might be surprised with inflight conditions. It would obviously need a slick airframe to go with it.
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I'm thinking about doing some tests that would simulate in flights conditions. That would be interesting for sure. I've read over and over that edf don't unload in flight, but I've already seen evidence that they do. The unloading might take the form of lower amp draw for the same rpm level instead of higher rpm, but my observation is that they do unload.
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Latest blog entry: EDF, My First Six Years, mostly Pictures
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Once upon a time...
Not saying EDF's should have just one blade but given a certain amount of watts to work with I would have that power turning fewer, high pitched blades as opposed to many lower pitched blades. Again, a very low drag airframe would be needed for a setup like that. |
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Hitting the nail on the head again lee! Now we all need to come up with a system of checking static in flight in line with efflux. Ie one might have gobs of static at full with efflux but! How much is left at half. And visa versa, tons of efflux but at speed how fast does that fall off. This was my next goal in life to create a load sensor setup for in flight, but alas sidelined with youngins right now so it has to wait.
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