Seastead Leg Structural Analysis

Objective: Determine the uniformly distributed lateral force a single leg can withstand before structural failure (yield/ultimate), and estimate the wave height required to generate that force.

Disclaimer: This is a preliminary engineering estimation based on simplified beam theory and linear wave theory (Morison equation). It does not account for dynamic amplification, slamming loads, stress concentrations at connections, fatigue, corrosion, or complex hydrodynamic diffraction effects. A full Finite Element Analysis (FEA) and Computational Fluid Dynamics (CFD) study by a certified naval architect is required for final design.

1. Leg Geometry & Assumptions

ParameterValueNotes
Length (L)21.5 ft (258 in)Total leg length
Submerged Length (Lsub)10.75 ft (129 in)Lower 50% (lower half in water)
Chord (c)8.5 ft (102 in)NACA 0035 foil chord
Max Thickness (tfoil)35% chord = 2.975 ft (35.7 in)NACA 0035 profile
Wall Thickness (tw)0.5 inMarine aluminum plate
Trailing EdgeBlunt (last 0.5 ft cut off)Fits 8.9 ft container height
Support ConditionFixed at top (welded to triangle frame), Free at bottomCantilever beam
Load DistributionUniform (evenly along leg)Analysis per user request

2. Material Properties (Marine Aluminum)

Alloy / TemperYield Strength (Fy)Ultimate Strength (Fu)Density
5086-H116 (Typical Marine)30 ksi (30,000 psi)40 ksi0.096 lb/in³
6061-T6 (Alternative)40 ksi45 ksi0.098 lb/in³

Calculations below use conservative 5086-H116 (Fy = 30 ksi, Fu = 40 ksi).

3. Cross-Section Properties (Simplified)

The NACA 0035 foil is modeled as a thin-walled closed section. The primary bending resistance comes from the top and bottom skins (flanges) separated by the foil thickness.

Note: This ignores the contribution of the leading/trailing edge skins, making it a conservative (lower bound) estimate.

4. Maximum Bending Moment Capacity

Myield = Fy × S = 30,000 psi × 1,820 in³ = 54,600,000 in-lbs = 4,550,000 ft-lbs
Multimate = Fu × Z = 40,000 psi × 2,730 in³ = 109,200,000 in-lbs = 9,100,000 ft-lbs