Finite Element Analysis (FEA) Matrix

FEA Simulation & Structural Stress Report
15m (50ft) Clear-Span Helicopter Maintenance Hangar - 50m Length

Exhaustive structural stress distribution matrix, maximum deflection limits (L/240), and site-specific wind pressure coefficients for Model hangar-15m-span-50m-len.

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Structural Analysis Disciplines

Engineered Limit State Verification for hangar-15m-span-50m-len

Clear Span Envelope15m (50ft) 100% Column-Free Span × 50m (164ft) 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)
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