◈ Flow Velocity
AIRSPEED U
0.0m/s
◈ Aeroelastic Section — Real-Time Simulation
— AIRFOIL
— FLAP
— STREAMLINES
◈ Controller
◈ Eigenvalue Map
● SYSTEM STABLE
◈ State Vector
h (m)
0.000
α (deg)
0.000
ḣ (m/s)
0.000
α̇ (°/s)
0.000
FLAP DEFLECTION β (deg)
0.000
◈ Time History
PLUNGE h (m)
PITCH α (deg)
FLAP β (deg)