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Split flap
What is a split flap? · Standard part · basis: Design rules and figures from the cited sources; example geometry by Xem Studio
Also called: split flaps, split flap rc, lower surface flap, intrados flap, split flap vs plain flap, dive flap, landing flap drag
Exact dimensions. True size, with no printing tolerance added.
- sizes
- 3 in table
Notes
- A split flap hinges down from the lower surface only, leaving the upper surface in place; it gives slightly more lift than a plain flap but high drag, and fully extended it adds high drag with little extra lift (FAA PHAK ch.6).
- That drag is useful for steep approaches. Arnedo groups the plain and 'intrados' (lower-surface) flap together at a section CLmax increment of about 0.9.
- 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.
Split flap size chart
| parameter | value or range | source |
|---|---|---|
| Section delta-CLmax (intrados flap) | 0.9 | Arnedo (Franchini) |
| Lift vs plain flap | slightly greater | FAA PHAK ch.6 |
| Reference build | chord 100, 25% lower-surface flap, 45 deg | illustrative |
Where the files are
Other publishers' files are linked, not hosted. "verify" = check the license at the link before commercial use.
| FAA | Pilot's Handbook of Aeronautical Knowledge (FAA-H-8083-25), Ch. 6 Flight Controls | web | Publisher's page; dimensions are facts |
| LibreTexts (Arnedo, Fundamentals of Aerospace Engineering; data from Franchini et al.) | 3.4.3 Increase in CLmax (high-lift devices) | web | Publisher's page; dimensions are facts |
Free files
★ Free files 1 parts. Xem Studio design: free to use, print and sell things from; not to be republished as files. Xem Studio Design License. index.json
| split-flap-wing-segment | split flap: wing segment 100 mm chord × 300 mm, 25 % chord surface deflected 45° | STEP · STL |
https://xemstudio.com/mcp to Claude, ChatGPT, Cursor or any MCP client (free, no account, one minute) and it can look up exact sizes, mating fits and free STEP/STL from every chat.Plain text: sheet.txt · JSON: /api/geometry?object=split-flap

Fits with
Questions
Why use a split flap on a model?
It is easy to add and gives high drag with a lift gain for steep landings (FAA PHAK ch.6).





