Asymptotic analysis of aircraft wing model in subsonic air flow

DOI10.1093/IMAMAT/66.4.319zbMath1053.76034OpenAlexW2005212867MaRDI QIDQ2764967

Marianna A. Shubov

Publication date: 2001

Published in: IMA Journal of Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1093/imamat/66.4.319

zbMATH Keywords

spectrumconvolution integral operatornon-selfadjoint differential operator

Mathematics Subject Classification ID

Asymptotic methods, singular perturbations applied to problems in fluid mechanics (76M45) General aerodynamics and subsonic flows (76G25) Asymptotic distributions of eigenvalues in context of PDEs (35P20)

Related Items (5)

Asymptotic distribution of the eigenvalues of the bending‐torsion vibration model with fully nondissipative boundary feedback ⋮ Riesz basis property of mode shapes for aircraft wing model (subsonic case) ⋮ Numerical investigation of aeroelastic mode distribution for aircraft wing model in subsonic air flow ⋮ Bending-torsion vibration model with two-end energy dissipation ⋮ Four-branch vibrational spectrum of double-walled carbon nanotube model

This page was built for publication: Asymptotic analysis of aircraft wing model in subsonic air flow