A Review of Computational Aeroelasticity Of Civil Fan Blades
Author:
Affiliation:
1. Department of Mechanical Engineering, Imperial College London
Publisher
Gas Turbine Society of Japan
Subject
Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jgpp/11/4/11_22/_pdf
Reference13 articles.
1. Vahdati, M., Sayma, A., Freeman, C. & Imregun, M. 2005 On the use of atmospheric boundary conditions for axial-flow compressor stall simulations. ASME. J. Turbomach. 127(3), 349-351
2. Vahdati, M, Sayma, A. I., Marshall, J. G., Imregun, M., 2001 Mechanisms and prediction methods for fan blade stall flutter. AIAA J of Propulsion & Power, 17(5), 1100-1108
3. Vahdati, M., Sayma, A. I., Breard, C., Imregun, M. 2002 A computational study of intake duct effects on fan flutter stability. The AIAA Journal, 40(3), 408-418
4. Zhao F, Smith N, Vahdati M. A Simple Model for Identifying the Flutter Bite of Fan Blades. ASME. J. Turbomach. 2017; 139(7):071003-071003-10. doi:10.1115/1.4035567
5. Stapelfeldt SC, Vahdati M, On the Importance of Engine-Representative Models for Fan Flutter Predictions, ASME. J. Turbomach. ISSN: 0889-504X
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