FUTURECRAFT

AI BASED CAD SYSTEM
ASSEMBLY STATUS 0/3 MODULES
WNG-01

Wings

CONFIG
MATERIALS & PHYSICS
STRUCTURAL COMPOSITION
MAT-SYS
DENSITY 2810 kg/m³
YIELD STR 503 MPa
MASS CALCULATION PROTOCOL
RAW VOL (GEOMETRY) 0.00 m³
× STRUCTURAL FILL 25%
Account for hollow structure (Ribs/Spars)
× MATERIAL DENSITY 2810 kg/m³
TOTAL EST. WEIGHT --- kg
PARAMETER CONTROLS
WING CONFIGURATION
WT-01
60.00 m
10m 50m 90m
14.00 m
3m 11m 20m
3.00 m
1m 3.5m 6m
30 deg
0 45 90
12 %
8 14 20
5 deg
-15 0 15
3D VIEWPORT
Wings
X 3.00
Y 2.00
Z 3.00

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