Flight report
One design in — full integrated report out. XFOIL section polar → stability → trim → performance.
One click fills in a complete, realistic design and runs the full report — no data entry needed. You can then tweak anything below and re-run.
Or build your own: pick an airfoil and cruise condition — the report runs the real XFOIL polar, anchors the wing lift slope to it, then computes stability, trim, dynamic modes, design checks, CG envelope and performance in one pass. Defaults match a typical LSA layout (edit the wing below).
Design & condition
Wing geometry (11.0 m span)
Tails, masses and control surfaces come from the selected example (or the LSA defaults). For full control over every surface, use Stability / Trim individually and combine via the Full report page.
Verdict
Run the report to see the integrated verdict — or click an example aircraft above to see a finished report instantly.