Pages that link to "Item:Q5933488"

The following pages link to Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model. (Q5933488):

Displaying 9 items.

• Bending-torsion vibration model with two-end energy dissipation (Q556049) (← links)
• Asymptotic theory of an oscillating wing section in weak ground effect (Q942231) (← links)
• Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow (Q966397) (← links)
• Parametric aeroelastic modeling based on component modal synthesis and stability analysis for horizontally folding wing with hinge joints (Q1798151) (← links)
• The transonic dip in aeroelastic divergence speed -- An explicit formula (Q1926327) (← links)
• Non-collocated boundary control for contact-force control of a one-link flexible arm (Q2181331) (← links)
• Asymptotic analysis of aircraft wing model in subsonic airflow (Q2717412) (← links)
• Asymptotic analysis of aircraft wing model in subsonic air flow. (Q2764967) (← links)
• Riesz basis property of mode shapes for aircraft wing model (subsonic case) (Q3503275) (← links)