Pages that link to "Item:Q2764967"
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The following pages link to Asymptotic analysis of aircraft wing model in subsonic air flow. (Q2764967):
Displaying 13 items.
- Bending-torsion vibration model with two-end energy dissipation (Q556049) (← links)
- Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow (Q966397) (← links)
- Asymptotic analysis of aircraft wing model in subsonic airflow (Q2717412) (← links)
- Subsonic aircraft's unsteady longitudinal stability derivatives calculation (Q2774621) (← links)
- Asymptotic behaviour of the aeroelastic modes for an aircraft wing model in a subsonic air flow (Q3022783) (← links)
- Asymptotic Analysis of Passive Nonlinear Suppression of Aeroelastic Instabilities of a Rigid Wing in Subsonic Flow (Q3053174) (← links)
- Four-branch vibrational spectrum of double-walled carbon nanotube model (Q3090250) (← links)
- (Q3154920) (← links)
- Riesz basis property of mode shapes for aircraft wing model (subsonic case) (Q3503275) (← links)
- Asymptotic and spectral properties of operator-valued functions generated by aircraft wing model (Q4458744) (← links)
- Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model. (Q5933488) (← links)
- Asymptotic representations for root vectors of nonselfadjoint operators and pencils generated by an aircraft wing model in subsonic air flow (Q5945096) (← links)
- Asymptotic distribution of the eigenvalues of the bending‐torsion vibration model with fully nondissipative boundary feedback (Q6068167) (← links)
