Pages that link to "Item:Q437158"
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The following pages link to An efficient method for nonlinear aeroelasticy of slender wings (Q437158):
Displaying 9 items.
- Linearization method of nonlinear aeroelastic stability for complete aircraft with high-aspect-ratio wings (Q546550) (← links)
- Semi-analytical static aeroelastic analysis and response of flexible subsonic wings (Q669663) (← links)
- Efficient nonlinear static aeroelastic wing analysis (Q1973762) (← links)
- A new correlation method for the aerodynamic service loads determination of a rigid wing based on CFD analysis (Q2290097) (← links)
- Nonlinear flutter and limit-cycle oscillations of damaged highly flexible composite wings (Q2296959) (← links)
- Least squares algorithm for an input nonlinear system with a dynamic subspace state space model (Q2436150) (← links)
- Iterative estimation methods for Hammerstein controlled autoregressive moving average systems based on the key-term separation principle (Q2439375) (← links)
- A New Dynamic Stall Approach for Investigating Bifurcation and Chaos in Aeroelastic Response of a Blade Section with Flap Free-Play Section (Q5138327) (← links)
- Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model. (Q5933488) (← links)
