Process / pipelineAeroelasticity

Theodorsen Flutter

Theodorsen flutter analysis is a classical aeroelastic method for predicting the onset of flutter, a self-excited oscillation where aerodynamic forces interact with elastic structural motion to cause rapid growth of oscillations. Developed by Theodore Theodorsen in 1935, the method uses frequency-domain analysis with Theodorsen's function to compute aerodynamic forces on oscillating wings. Flutter speed prediction is essential for aircraft certification and structural design.

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Sources

  1. Theodorsen, T. (1935). General theory of aerodynamic instability and the mechanism of flutter. NACA Report No. 496. link
  2. Bisplinghoff, R. L., Ashley, H., & Halfman, R. L. (1955). Aeroelasticity. Addison-Wesley. link
  3. Wright, J. R., & Cooper, J. E. (2007). Introduction to Aircraft Aeroelasticity and Loads (2nd ed.). John Wiley & Sons. DOI: 10.1002/9780470693766

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Referenced by

ScholarGateTheodorsen Flutter (Theodorsen Flutter Analysis). Retrieved 2026-06-04 from https://scholargate.app/en/aerospace/theodorsen-flutter