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1 Geometry
3 Meshes
3 Simulation setups
3 ResultsA10_C QC-held +7 wing structural analysis. Twist A and 41-rib loft signed. Current spar law: front FS181.7685 constant; rear FS202.1347 through Y74.299, then LE + 0.47828 local chord. 3400-lb design / 3800-lb structural sensitivity. Analysis only. ZERO fabrication / ZERO flight release.
by slilbaekslilbaek
brentbond81120 created this project
25 days ago
1 Geometry 3 Meshes 3 Simulation setups 3 ResultsA10_C QC-held +7 wing structural analysis. Twist A and 41-rib loft signed. Current spar law: front FS181.7685 constant; rear FS202.1347 through Y74.299, then LE + 0.47828 local chord. 3400-lb design / 3800-lb structural sensitivity. Analysis only. ZERO fabrication / ZERO flight release.
