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Asymptotic Representations for Root Vectors of Nonselfadjoint Operators and Pencils Generated by an Aircraft Wing Model in Subsonic Air Flow

  • Published:2001-08 Issue:2 Volume:260 Page:341-366
  • ISSN:0022-247X
  • Container-title:Journal of Mathematical Analysis and Applications
  • language:en
  • Short-container-title:Journal of Mathematical Analysis and Applications

Author:

Shubov Marianna A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Analysis

Reference28 articles.

1. Sobolev Spaces;Adams,1975

2. Engineering Analysis of Flight Vehicles;Ashley,1992

3. Aerodynamics of Wings and Bodies;Ashley,1985

4. Aeroelastic control with self-straining actuators: continuum models;Balakrishnan,1998

5. Subsonic flutter suppression using self-straining actuators;Balakrishnan;J. Franklin Inst.,2001

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1. Asymptotic distribution of the eigenvalues of the bending‐torsion vibration model with fully nondissipative boundary feedback;Studies in Applied Mathematics;2023-01-26

2. On fluttering modes for aircraft wing model in subsonic air flow;Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences;2014-12-08

3. Numerical Investigation of Aeroelastic Mode Distribution for Aircraft Wing Model in Subsonic Air Flow;Mathematical Problems in Engineering;2010

4. Sums of characteristic values of compact polynomial operator pencils;Journal of Mathematical Analysis and Applications;2008-02

5. Flutter Phenomenon in Aeroelasticity and Its Mathematical Analysis;Journal of Aerospace Engineering;2006-01
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