CFD for turbomachinery unsteady flows - An aeroelastic design perspective
Author:
Affiliation:
1. GE Aircraft Engines, Cincinnati, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-429
Reference7 articles.
1. A Design Method to Prevent Low Pressure Turbine Blade Flutter
2. Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan
3. Marshall, J. G., Denton, J., Xu, L., and Chew, J. W., 2000, Prediction of Low Engine Order Inlet Distortion Driven Resonance in a Low Aspect Ratio Fan, ASME Paper 2000-GT-0374
4. Breard, C., Vahdati, M., Sayma, A. I., and Imregun, M., 2000, An Integrated Time-Domain Aeroelasticity Model for the Prediction of Fan Forced Response Due to Inlet Distortion, ASME Paper 2000-GT-0373
5. Weaver, M. W., Manwaring, S. R., Abhari, R. S., Dunn, Salay, M. J., Frey, K. K., Heidegger, N., 2000, Forcing Function Measurements and Predictions of a Transonic Vaneless Counter Rotating Turbine, ASME Paper 2000-GT-375
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1. Forced Response Sensitivity Analysis Using an Adjoint Harmonic Balance Solver;Journal of Turbomachinery;2019-01-21
2. The Influence of Steady Loading Parameters on Low-Pressure Turbine Flutter;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02
3. Physical Understanding and Sensitivities of Low Pressure Turbine Flutter;Journal of Engineering for Gas Turbines and Power;2014-08-26
4. A COUPLED FLUID–STRUCTURE ANALYSIS FOR 3-D INVISCID FLUTTER OF IV STANDARD CONFIGURATION;Journal of Sound and Vibration;2002-03
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