Calculation of Wing Flutter Using Euler Equations with Approximate Boundary Conditions

  • Biao Zhu
  • Zhide Qiao
Conference paper

Abstract

Aeroelastic simulation, such as flutter prediction, is an important issue for modern aircraft design. If flutter occurs during flight, it will be lead to disastrous structural failure. So flutter is a catastrophic aeroelastic phenomenon that all flight vehicles must be clear of in their flight envelope.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2009

Authors and Affiliations

  • Biao Zhu
    • 1
  • Zhide Qiao
    • 1
  1. 1.National Key Laboratory of Aerodynamic Design and ResearchXi’anChina

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