02 / 3D Modelling
Aircraft StudioFrom form to function.
Explore the airframe, separate its assemblies and look inside the engine.
Wing area62.37 m²
Aspect ratio7.76
Tip width1.47 m
AS-01 is a conceptual business jet, not a certified aircraft. Geometry is editable; flight performance is a separate calculation.
Geometry & limitations
Wing area = span × (root width + tip width) / 2. Aspect ratio = span² / wing area. The reference area includes the wing inside the body and excludes winglets.
This is a conceptual geometry study, not structural analysis, CAD or CFD. Changing sweep, paint or body length does not calculate fuel efficiency, stability or a new lift coefficient.
Reference: NASA wing geometry