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The Air Flow Model/Boundary Fluid Structure Interaction/The Aeroelastic Problem

  • A V Balakrishnan
Chapter

Abstract

In this chapter we make a precise mathematical statement of the aeroelastic problem that we wish to solve. Having described the structure model, we turn to the air flow model simplifying it to the most used case where we neglect viscosity and consider “nonviscous flow” but more importantly assume that the entropy is constant. This makes the flow vortex free so that the flow can be described in terms of the potential. Our concern is again more the structure response in air flow—“aeroelasticity”—and hence the fluid–structure boundary conditions play the dominant role in determining the aerodynamic loading on the wing structure.

Keywords

Aerodynamic Loading Flutter Speed Wing Structure Isentropic Flow Aeroelastic Problem 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media, LLC 2012

Authors and Affiliations

  • A V Balakrishnan
    • 1
  1. 1.Department of Electrical Engineering Department of MathematicsUniversity of CaliforniaLos AngelesUSA

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