Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow

DOI10.1155/2010/879519zbMath1191.76082OpenAlexW2045737223WikidataQ58653396 ScholiaQ58653396MaRDI QIDQ966397

B. E. Eshmatov

Publication date: 23 April 2010

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://eudml.org/doc/226496

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Related Items (2)

Asymptotic distribution of the eigenvalues of the bending‐torsion vibration model with fully nondissipative boundary feedback ⋮ Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow

Cites Work

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• Spectral analysis of coupled Euler-Bernoulli and Timoshenko beam model
• Asymptotic and spectral properties of operator-valued functions generated by aircraft wing model
• A note on Riesz bases of eigenvectors of certain holomorphic operator-functions
• Subsonic flutter suppression using self-straining actuators
• Asymptotics of aeroelastic modes and basis property of mode shapes for aircraft wing model.
• Asymptotic representations for root vectors of nonselfadjoint operators and pencils generated by an aircraft wing model in subsonic air flow

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