Leading-edge cuff (drooped leading edge) — dimension sheet Source: Xem Studio, https://xemstudio.com/objects/leading-edge-cuff/ (sheet CC BY 4.0; files Xem Studio Design License, https://xemstudio.com/license/) Basis: Design rules and figures from the cited sources; example geometry by Xem Studio Catalog version: 2026-10-20 Sizes: see table below - A cuff extends the leading edge down and forward, lowering stall speed at a cruise-speed penalty (FAA PHAK ch.6). - On NASA's canard GA model an outboard droop of about 6% chord extension and 3% camber over the outer 25% of span stopped premature tip stall, increased roll damping and eliminated wing rock; without it roll damping went unstable near 16 deg (NASA TP-2623). - The reported cruise drag penalty was 0.0040 (NASA TP-2623, citing reference data). - Used on: NASA canard GA model (TP-2623). - The file is a reference example built by Xem Studio from the numbers above. Sizes the sources do not fix are illustrative; scale the example to your own vehicle. parameter value or range source Outboard droop geometry ~6% chord extension, ~3% camber, outer 25% span NASA TP-2623 Roll damping without droop unstable at ~16 deg AoA NASA TP-2623 Cruise drag penalty 0.0040 NASA TP-2623 Reference build chord 100, 6% extension on 25% of a 1200 span NASA TP-2623 Files elsewhere (not hosted by Xem Studio; license as stated by the publisher): - FAA: Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25), Ch. 6 Flight Controls — web — Publisher's page; dimensions are facts — https://www.faa.gov/sites/faa.gov/files/08_phak_ch6.pdf - NASA Langley (D. Satran): Wind-Tunnel Investigation of the Flight Characteristics of a Canard General-Aviation Airplane Configuration, NASA TP-2623 (1986) — web — Publisher's page; dimensions are facts — https://ntrs.nasa.gov/api/citations/19870000606/downloads/19870000606.pdf Free files (Xem Studio Design License, Xem Studio; STEP + STL, 1 parts): https://xemstudio.com/files/hardware/leading-edge-cuff/index.json API: https://xemstudio.com/api/geometry?object=leading-edge-cuff