Reduction of boundary value problem to Possio integral equation in theoretical aeroelasticity
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Publication:937498
DOI10.1155/2008/846282zbMath1142.76028OpenAlexW2133956803WikidataQ58645969 ScholiaQ58645969MaRDI QIDQ937498
A. V. Balakrishnan, Marianna A. Shubov
Publication date: 15 August 2008
Published in: Journal of Applied Mathematics (Search for Journal in Brave)
Full work available at URL: https://eudml.org/doc/54412
Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) General aerodynamics and subsonic flows (76G25) Integral equations with kernels of Cauchy type (45E05)
Related Items (2)
Asymptotic representation for the eigenvalues of a non-selfadjoint operator governing the dynamics of an energy harvesting model ⋮ Static stability analysis of a thin plate with a fixed trailing edge in axial subsonic flow: Possio integral equation approach
Cites Work
- Studies of store-induced limit-cycle oscillations using a model with full system nonlinearities
- The Possio Integral Equation of Aeroelasticity: A Modern View
- Asymptotic behaviour of the aeroelastic modes for an aircraft wing model in a subsonic air flow
- Riesz basis property of mode shapes for aircraft wing model (subsonic case)
- Shear flow aerodynamics - Lifting surface theory
- Variable thickness shear layer aerodynamics revisited
- Aerodynamic Effects of Inviscid Parallel Shear Flows
- Subsonic flutter suppression using self-straining actuators
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