AEROELASTIC INSTABILITY
TACOMA FLUTTER ENGINE
// TORSIONAL FLUTTER & VON KÁRMÁN VORTEX SHEDDING
⚙ Open Settings
Parameters
LAMINAR REGIME
✕
BRIDGE AERODYNAMICS
Damping (ζ)
0.010
Stiffness (Kθ)
1.0x
Crosswind (V)
0 km/h
VORTEX FREQ (fs)
0.00 Hz
NATURAL TORSION (f0)
0.20 Hz
TORSION ANGLE (θ)
0.0°
FLUTTER STRESS (τ)
0 MPa
YIELD LIMIT
240 MPa
🔄 RECONSTRUCT BRIDGE
CATASTROPHIC COLLAPSE
TORSIONAL FLUTTER INSTABILITY THRESHOLD SURPASSED
CELCALC KINEMATICS