| ▲ | dyauspitr 2 hours ago | |||||||
Hunh so for pure lifting our standard helicopter design is apparently the best. How did we stumble on the perfect design half a century ago? Was it sheer luck and constraints or can you actually do the math for this to work it out? | ||||||||
| ▲ | regularfry 2 hours ago | parent | next [-] | |||||||
The article makes reference to this being expected from the physics, but I don't think it's particularly intuitive why it should be the case. Unless it's as simple as smaller swept areas needing higher tip speeds for the same lift? That would make the energy loss to drag worse for multirotors. | ||||||||
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| ▲ | somat an hour ago | parent | prev | next [-] | |||||||
I am surprised it was not a coaxial design(think the mars copter, but designed for a real atmosphere) | ||||||||
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| ▲ | whatever1 2 hours ago | parent | prev | next [-] | |||||||
We have also achieved optimal teapot design for perfect flow thousands of years ago. We have some times very good intuition and ideas. | ||||||||
| ▲ | ballooney 39 minutes ago | parent | prev [-] | |||||||
For a given lift, a larger, lower speed rotor is strictly more efficient than a smaller faster one, all else being equal. So no surprises that when efficiency matters we don’t see quadcopter-type designs. The reason they became ubiquitous is because they are so mechanically simple, all the control can be done with cheap electronics, no need for the great mechanical complexity of a swashplate. | ||||||||