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Community submission — not verified by nTop. This package was submitted by an outside community member and has not been reviewed or verified by nTop. Treat its accuracy, safety, and compatibility claims with appropriate caution.
Summary
Inspect the native Fury RC appearance study with finite trailing edges, editable loft guides, and retained mesh-readiness lessons.Package Details
Built with Astra. Inspect the native Fury RC appearance study with finite trailing edges, editable loft guides, and retained mesh-readiness lessons.
The primary notebook has 0.5 inch full trailing-edge thickness on the wing, horizontal tail, and fin. Meshing and exports remain paused. Earlier appearance and layout notebooks are included with explicit earlier filenames. The linked algorithmic builder reconstructs the earlier baseline. Recorded mesh defects remain unresolved.
Installation and use
- Download the package files and keep them together.
- Open
fury-rc-finite-edges.ntopin the matching licensed nTop build. - Save a working copy before editing. Expand the relevant section and change one control at a time.
- Inspect the rebuilt bodies and block states before accepting the changed model.
Inputs and outputs
Named scalar controls include
RC wingspan, RC scale factor, Fuselage width multiplier, Fuselage height multiplier, Inlet lower depth multiplier, Upper conic rho adjustment, Inlet lip forward projection, Inlet lip thickness, Inlet lip center gap, Gap splitter start station, Gap splitter aft station, Gap splitter inlet-roof offset. Some are computed values; inspect their upstream construction before changing them.
Files
- fury-rc-finite-edges.ntop
- earlier-appearance.ntop
- earlier-internal-layout.ntop
- earlier-gear-illustration.ntop

