Whole-Assembly Flutter Analysis of a Low Pressure Turbine Blade

Author:

Sayma A. I.,Vahdati M.,Green J. S.,Imregun M.

Publisher

Springer Netherlands

Reference13 articles.

1. E. Goldstein, W. Braun and J. J. Adamczyk(1977), Unsteady flow in supersonic cascade with strong in-passage shocks, J. Fluid Mech. 83, 569–604.

2. O. O. Bendiksen(1986), Role of shocks in transonic/supersonic compressor rotor flutter, AIAA Journal 24, 1179–1186.

3. M. Vahdati and M. Imregun(1995), Non-linear aeroelasticity analyses using unstructured dynamic meshes, In Y. Tanida and M. Namba (eds.), Unsteady Aerodynamics and Aeroelasticity of turbomachines, Elsevier Pubbblishers, pp. 177-190.

4. K. Morgan, J. Peraire and J. Peiró, Unstructured grid methods for compressible flow, AGARD Report 787, Special Course on Unstructured Grid Methods for Advection Dominated Flows.

5. B. S. Baldwin and. J. Barth(1991), A one equation turbulence transport model for high Reynolds number wall-bounded flows, AIAA Paper 91-0610.

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Experimental Validation of Numerical Blade Flutter Prediction;Journal of Propulsion and Power;2015-09

2. Semi-Unstructured Mesh Generator for Flow Calculations in Axial Turbomachinery Blading;Unsteady Aerodynamics and Aeroelasticity of Turbomachines;1998

3. FLUTTER BOUNDARIES FOR PAIRS OF LOW PRESSURE TURBINE BLADES;UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES

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