Skip to main content
11 events
when toggle format what by license comment
Aug 14, 2019 at 15:04 vote accept Fred
Aug 4, 2019 at 13:50 history edited JZYL CC BY-SA 4.0
OP modified to state slotted elevator rather than "slatted elevator"
Aug 3, 2019 at 20:47 comment added JZYL @Fred Your OP mentioned "slatted elevator". I think you meant "slotted elevator". I've submitted a change to your OP to reflect this.
Aug 2, 2019 at 14:09 comment added Fred I'm pretty sure this is a slotted flap. The max cL of a slotted flap is 1.5 cL base plus 1.3 cL for the slotted flap, for a total of 2.8 max cL, which is exactly the number Zenith is giving.
Jul 29, 2019 at 17:05 comment added JZYL @Fred I think you mean an elevator where the hinge line allows a certain air gap (that's not a slat)? Most powered planes have sealed hinge lines to improve elevator authority limits. By one account, on a particular airplane model, the air gap (unsealed) seems to have helped. But I don't think this is a universal phenomenon and is model/profile dependent.
Jul 29, 2019 at 15:55 comment added Fred See zenithair.com/stolch801/design/design.html. for their venturi/slotted elevator, near zero drag slats, low speed flaps, etc.
Jul 27, 2019 at 16:51 comment added JZYL @Fred Where do you see they use a slotted elevator? On their design page, I only see slotted LE on the wing.
Jul 27, 2019 at 16:32 comment added Fred Zenith uses a slotted elevator to generate as much downforce as possible, so they can ascend or descend at an AOA of 30 deg for STOL purposes with elevator deflections of 40 deg!!
Jul 27, 2019 at 16:19 comment added JZYL @Fred tail stall occurs at negative tail incidence angle. Why do you think a slotted flap on tail helps?
Jul 27, 2019 at 16:16 comment added Fred Perhaps a better description would be a slotted flap which would increase the cL max from 2.2 to about 2.8!!
Jul 26, 2019 at 4:21 history answered JZYL CC BY-SA 4.0