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| Aerodynamics What makes 'em fly? Designs & technology related to aerodynamics. |
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| | #1 (permalink) |
| Gettin' Lower! ![]() | `I have been involved in IMAC for some few years now and have seen some airframes outfitted with a rather sharp leading edge at the tip and as it makes it way to the root it transituions gradually to the conventional rounded profile. I was of the impression that this was a useful design element to assist spin/snap entry. Is this still a viable design when we consider todays airframes?? MIke Sotomayor THE Staudman Miguel Sotomayor THE Staudmans Builder !!! |
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| | #2 (permalink) |
| I had it, but then I lost it. ![]() | I'm not sure but I had a friend experement with something similar. He taped a piece of tri stock to the LE. He said it helped to be more precise in rolls and such.
__________________ "In memory of Sean Branson" |
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| | #3 (permalink) |
| Bad-ass Super Contributer! ![]() | sharper is faster on pitch changes and not quite as stable on a straight flyby if you wiggle the sticks at all.rounded is more forgiving and smoother on pitch changes,that is why most good imac planes do not have a sharp leading edge
__________________ Life's journey is not to arrive at the grave >safely and in a well preserved body,but rather to skid in > sideways,totally screwed up,worn out,shouting,"oh damn what a fine ride! AMA 98634 > LOOKS LIKE SINGLE LIFE IS A COMIN > Futaba, FROMECO:a good way to get a charge out of life My avitar says it all.3w all the time ![]() |
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| | #5 (permalink) | ||||||||||||||||||
| Old School Hucker ![]() |
A sharp leading edge WILL allow the airflow to detach quicker making snap entries a bit sharper. It still takes the same angle of attack to depart, but when it reaches critical AoA, the flow detaches MUCH faster with a shapened leading edge. | ||||||||||||||||||
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| | #6 (permalink) |
| doin' it ![]() | Shaker is right. Take a look at Abbott and Von Doenhoff data. The thickness of an airfoil affects post stall characteristics. That is, after the airfoil reaches max lift/aoa. For a given airfoil of varying thickness both are the same. |
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