Flutter stability analysis of a complete fan assembly

Author:

Breard C.1,Imregun M.1,Sayma A.1,Vahdati M.1

Affiliation:

1. Imperial College of Science, Technology and Medicine, London, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. A modified segmentation approach for analyzing plane wave propagation in non-uniform ducts with mean flow

2. Nayfeh, A. H., Kaiser, J. E. & Shaker, B. S., 1979, A wave envelop analysis of sound propagation in non-uniform circular ducts with compressible mean flows. NASA contractor 3109 Report

3. Nayfeh, A. H. Shaker, B. S. & Kaiser, J. E. 1980, Transmission of sound through nonuniform circular ducts with compressible mean flows AIAA Journal, Vol.18, pp515-525.

Cited by 1 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

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