WebCAE
WebCAE PlatformUnified FEA & CFD simulation platform: Browser WebAssembly + Native Desktop

Inspect pre-solved models in your browser in 2 seconds (up to 300k DOF) or solve 1.5M+ DOF assemblies 100% offline on Windows and macOS.

Browser WASM
Up to 300k DOF · 2s load
Native Desktop (Pro)
Up to 1.5M+ DOF · 100% offline
Physics & Solvers
Static, Modal, Kσ, Contact, CFD
Observation Tower · 184 m · Flying Saucer HaloCivil & BridgesMITC4 Shells & Beams

Seattle Space Needle: 184 m Tripod Tower & Flying Saucer Halo

6 curved tubular steel legs, pinch waist profile, central elevator core, 42 m flying saucer halo, and aircraft spire.

Verify lateral deflection and modal vibration frequencies of the slender waist under hurricane-force wind loads, ensuring cantilever brackets supporting the heavy revolving restaurant halo maintain structural integrity.

✓ Curved Leg Axial & Bending Interaction✓ Cantilever Saucer Halo Outrigger Load Transfer✓ Pacific Northwest Wind Gust Dynamic Sway✓ Slender Tripod Waist Eigenvalue Buckling
Pre-solved .caeweb container ready
6 Curved Steel Legs · 184 m · 42 m Saucer Disk · Gale-force wind & seismic design
Open in Web App (WASM) →
Opens directly on the Results tab in 2 seconds without re-solvingNeed 1.5M+ DOF offline? Get Pro ↓
Seattle Space Needle: 184 m Tripod Tower & Flying Saucer Halo
6 Curved Steel Legs · 184 m · 42 m Saucer Disk · Gale-force wind & seismic designLaunch 3D ↗
Total Height
184 m
Tripod Legs
6 Curved Steel Box Legs (3 Pairs)
Waist Diameter
Ø 15 m (at z = 110 m)
Halo Diameter
Ø 42 m (z = 150..164 m)

1. Geometry & FEA Mesh

  • •6 curved tubular steel legs arranged in 3 symmetric pairs, curving from base radius R = 22 m to waist R = 7.5 m (at z = 110 m) and expanding to R = 10.5 m (at z = 150 m)
  • •Central triangular steel lattice elevator core tied to the legs by 4 levels of horizontal belt trusses (z = 35, 70, 105, 140 m)
  • •Cantilevered 5-storey flying saucer halo (diameter D = 42 m) at z = 150 to 164 m with radial truss outriggers
  • •Top observation spire and aircraft beacon mast rising from z = 164 m to 184 m

2. Loads & Boundary Conditions

  • •Fixed anchor supports at the 6 leg foundation bases at ground z = 0
  • •Self-weight gravity with heavy restaurant deck and machinery loads
  • •Pacific Northwest gale wind pressure along +X acting on legs, core, and 42 m saucer disk

3. Simulation Results & Findings

  • ✓Tripod curved leg geometry creates exceptional lateral stiffness with low sway amplitude
  • ✓Fundamental sway mode f₁ reflects well-balanced mass and stiffness distribution
  • ✓Buckling analysis validates stability of the curved compression legs against lateral-torsional buckling
Enterprise & Engineering Workflow

Rapid validation of iconic tower geometries, tripod structures, and cantilevered observation disks in a free browser CAE platform.

Launch Case in Web App →
14-Day Free Trial · $0 Due Today
$99/ mo (billed monthly after 14-day trial)

14 days of full Pro access. The first charge occurs only after 14 days unless canceled beforehand.

  • ✓14-Day Trial ($0 Today) (cancel anytime)
  • ✓Up to 1.5M+ DOFs (direct sparse solver)
  • ✓Native Windows & macOS Apps (100% offline)
  • ✓Nonlinear Contact & Buckling (Kσ, MITC4, RBE2/RBE3)

$0 due today. First charge occurs in 14 days unless cancelled. Cancel anytime in 1 click in your account.

Need bespoke solver development or a Dedicated Cloud VPS (128+ GB RAM, 32 cores)?
We build turnkey industry FEA pipelines and custom material models for engineering teams.

Ask an Engineer About Your Model

Describe your part, load case, or CAD format — we reply within 2 business hours.

WebCAE AI Assistant in bottom-right ↘

Want an instant answer on FEA theory or this model?

Click the AI chat button in the bottom-right corner to ask about boundary conditions, stress criteria, mesh convergence, or DSL scripting.

We use essential cookies to run this site, plus analytics cookies if you agree. Privacy Policy