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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 R6 aircraft appearance study with fair airfoils, revised aft-fuselage guides, and finite trailing edges.Package Details
Built with Astra. Inspect the R6 aircraft appearance study with fair airfoils, revised aft-fuselage guides, and finite trailing edges.
The saved graph preserves R6 geometry and editable controls. Earlier cross-CAD comparisons use R3 and must not be treated as R6 measurements. Replay does not repeat the original fitting process.
Installation and use
- Download the package files and keep them together.
- Open
f16-fair-airfoils-r6.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
Wingspan, Scale factor, Fuselage width multiplier, Fuselage height multiplier, Canopy height multiplier, Wing thickness multiplier, Trailing edge thickness at 32 ft, Normalized trailing edge thickness, Wing tip chord multiplier, Wing tip twist slope, Tail thickness multiplier, Fin thickness multiplier. Some are computed values; inspect their upstream construction before changing them.