Pages that link to "Item:Q966397"

The following pages link to Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow (Q966397):

Displaying 8 items.

• Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow (Q966397) (← links)
• Aeroelastic stability of a wing with bracing struts (Keldysh problem) (Q1288569) (← links)
• The new airfoil model NACA0015, modal analysis and flutter properties (Q2281931) (← links)
• Asymptotic analysis of aircraft wing model in subsonic air flow. (Q2764967) (← links)
• Asymptotic Analysis of Passive Nonlinear Suppression of Aeroelastic Instabilities of a Rigid Wing in Subsonic Flow (Q3053174) (← links)
• Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds (Q4794142) (← links)
• Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model. (Q5933488) (← links)
• Asymptotic distribution of the eigenvalues of the bending‐torsion vibration model with fully nondissipative boundary feedback (Q6068167) (← links)