Flutter and Modal Analysis of Gas Turbine Compressor Blades
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-16-0159-0_62
Reference10 articles.
1. Kielb, R., Barter, J., Chernysheva, O., & Fransson, T. (2006). Flutter design of lowpressure turbine blades with cyclic symmetric modes. unsteady aerodynamics, aeroacoustics and aeroelasticity of turbomachines, 41–52
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3. Panovsky J, Kielb RE (1998). A design method to prevent low pressure turbine blade flutter. In: Proceedings of the manufacturing materials and metallurgy; ceramics; structures and dynamics; controls, diagnostics and instrumentation; education, vol 5
4. Lee BHK, Liu L, Chung KW (2005) Airfoil motion in subsonic flow with strong cubic nonlinear restoring forces. J Sound Vib 281(3–5):699–717
5. Chung KW, Chan CL, Lee BHK (2007) Bifurcation analysis of a two-degree-of-freedom aeroelastic system with freeplay structural nonlinearity by a perturbation-incremental method. J Sound Vib 299(3):520–539
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