Finite Element Analysis (FEA) Matrix

FEA Simulation & Structural Stress Report
42m (140ft) Clear-Span Airbus A320 Base Overhaul Hangar - 35m Length

Exhaustive structural stress distribution matrix, maximum deflection limits (L/240), and site-specific wind pressure coefficients for Model hangar-42m-span-35m-len.

Request Stamped Calculation PDF View Product Specifications →
Structural Analysis Disciplines

Engineered Limit State Verification for hangar-42m-span-35m-len

Clear Span Envelope42m (140ft) 100% Column-Free Span × 35m (114ft) Continuous Hangar Bay
Design Code StandardASCE 7-16 / Eurocode EN 1991 / IBC 2021
Maximum Stress Ratio (D/C)< 0.82 (Governed by wind uplift and lateral shear)
Deflection Limit SLSVertical L/240, Horizontal Lateral Drift H/150
FEA Software ModelingSAP2000 / ANSYS Structural / RFEM 6
Manufacturing GroupSpanbest Industry Co., Ltd. (Hunan Champion & Guangzhou Tentsen)
Download Signed PE Calculation Document →