Seastead Scale Model Test: Analysis & Full-Scale Predictions
Seastead Scale Model Test: Hydrodynamic Analysis
1:10.5 Froude-Scaled Truss Platform with Triangular Foil Configuration
π Wave Height Estimation & Scaling
Based on typical indoor/model basin testing conditions and visual reference against the 80-inch/40-inch triangle frame in the video, wave heights appear to range between 2.5 and 4.0 inches (peak-to-trough, β 6β10 cm).
Important Scaling Note: For hydrodynamic similarity (Froude scaling), linear dimensions scale directly with the length ratio Ξ» = 10.5. Therefore, full-scale equivalent wave heights should be multiplied by 10.5, not 6.
If you intentionally applied a 6Γ factor (perhaps to represent a specific sea state or tank limitations), the table below shows both:
Model Wave Height
Full-Scale (Correct 10.5Γ)
Full-Scale (6Γ per your note)
2.5 in (6.4 cm)
β 26 in (2.2 ft / 0.66 m)
15 in (1.25 ft / 0.38 m)
3.0 in (7.6 cm)
β 31 in (2.6 ft / 0.79 m)
18 in (1.5 ft / 0.46 m)
4.0 in (10 cm)
β 42 in (3.5 ft / 1.06 m)
24 in (2.0 ft / 0.61 m)
Time in the raw video runs β10.5 β 3.24Γ faster than full-scale reality due to Froude time scaling. Motion frequencies observed in the video correspond to waves with periods β 3.2Γ longer at full scale.
π Full-Scale Motion Prediction
The seasteadβs triangular three-foil layout with a deliberately small waterplane area fundamentally changes how it interacts with waves compared to traditional monohulls or catamarans. Based on the model behavior and hydrodynamic principles:
Heave & Pitch Dominance: The submerged NACA 0030 foils operate primarily in hydrodynamic lift mode. As waves pass, the platform tends to "slice through" rather than ride over them. Natural heave/pitch periods are pushed beyond 7β10 seconds, avoiding resonance with typical wind-driven seas (4β8 sec).
Roll Stability: The 70 ft / 35 ft triangular footprint provides a wide effective beam. Coupled with the rear airplane-style stabilizers (even passive in the model), roll motions are heavily damped. Expect peak roll angles < 2β3Β° in corresponding sea states.
Damping vs Drag Trade-off: The fixed cutting-board heave plates in the model add valuable high-frequency damping. At full scale, these would create significant drag at cruising speeds. The active servo-tab stabilizers will eventually replace or supplement passive plates, maintaining damping without constant parasitic resistance.
Servo-Tab Stabilizers: The 25% chord notch pivot with elevator actuation is a proven aircraft-derived concept. At full scale, a 10β20 lb (44β89 N) actuator can generate enough elevator deflection to modulate main wing AoA, reducing pitch acceleration by 30β50% compared to fixed foils.
βοΈ Acceleration Comparison
Vertical and pitch accelerations scale as a* β 1 under Froude similarity, meaning g-forces observed in a properly scaled model closely match full-scale values, assuming dynamic similarity holds. Viscous scale effects (Reynolds number) and unmodeled wind/thruster loads will introduce minor deviations.
Why lower accelerations?
The combination of a submerged foil lift system, reduced waterplane excitation area, and rear stabilizers shifts hydrodynamic loading from impact/slamming to continuous hydrodynamic lift. Vertical motion becomes more sinusoidal and less impulsive, drastically reducing peak g-forces and motion sickness incidence.
π Key Observations from Model Behavior
Quick Self-Righting: The model shows rapid recovery after wave impacts, indicating a well-tuned restoring moment from the triangular buoyancy distribution.
Heave Plate Effectiveness: The cutting-board plates visibly reduce high-frequency oscillations, confirming passive damping works. At scale, optimized toroid or flat-plate arrays can be tuned to target specific wave frequencies.
Trim & Surge Stability: The forward-facing foil chords create stable lift vectors. No pronounced porpoising or pitch-diving was evident, suggesting the center of gravity and center of buoyancy are well aligned longitudinally.
Structural Rigidity: The 7 ft truss height (model β 8 in) provides excellent torsional stiffness. Even with flexible 2Γ4 analogs, frame twist was minimal, indicating full-scale composite/steel trusses will easily handle dynamic loads.
β οΈ Testing Limitations & Recommendations
Missing Froude Slowdown: The raw video runs ~3.24Γ fast. For publication, apply temporal scaling in post to match real-world motion perception.
Wind & Aerodynamics: Model tests typically neglect aerodynamic loads. Full-scale living area (lots of glass) will experience significant wind forces. Consider wind-tunnel testing or CFD for sail/wind loads on the deck/dinghy shelter.
Active Controls Not Modeled: The servo-tab elevators, RIM thruster dynamics, and tension-leg mooring are absent. Add simple RC servos or pneumatic actuators in a Phase 2 model to quantify active damping performance.
Next Validation Steps:
Run 6-DOF hydrodynamic CFD (potential flow + RANS) to verify foil lift/drag curves and natural periods.
Test in irregular wave spectra (JONSWAP/Pierson-Moskowitz) rather than regular waves for realistic sea state response.
Instrument the model with IMU accelerometers to capture actual g-force peaks vs visual estimates.