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.
Zdrojový záznam
Citácie skopírované doslovne zo zdrojového záznamu metódy. Nevyplýva z nich žiadne overenie na úrovni tvrdenia.
- Theodorsen, T. (1935). General theory of aerodynamic instability and the mechanism of flutter. NACA Report No. 496. · URL
- Bisplinghoff, R. L., Ashley, H., & Halfman, R. L. (1955). Aeroelasticity. Addison-Wesley. · URL
- Wright, J. R., & Cooper, J. E. (2007). Introduction to Aircraft Aeroelasticity and Loads (2nd ed.). John Wiley & Sons. · DOI 10.2514/4.479359
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Súvisiace metódy
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