Pages that link to "Item:Q3425341"
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The following pages link to A comparison of full non-linear and reduced order aerodynamic models in control law design using a two-dimensional aerofoil model (Q3425341):
Displaying 3 items.
- Support-vector-machine-based reduced-order model for limit cycle oscillation prediction of nonlinear aeroelastic system (Q1954481) (← links)
- Limit cycle oscillation prediction and control design method for aeroelastic system based on new nonlinear reduced-order model (Q2845373) (← links)
- Global sensitivity analysis for mathematical models comparison (Q6184777) (← links)