Use of finite element techniques in the determination of the acoustic properties of turbofan inlets
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Ga.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-18
Reference18 articles.
1. The acoustics of aircraft engine-duct systems
2. Transmission of spinning acoustic modes in a slightly non-uniform duct
Cited by 12 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. A finite element method for computing sound propagation in ducts;Mathematics and Computers in Simulation;1987-02
2. An iterative method for predicting turbofan inlet acoustics;AIAA Journal;1982-12
3. Accuracy and stability of finite element schemes for the duct transmission problem;7th Aeroacoustics Conference;1981-08-17
4. Applications of Velocity Potential Function to Acoustic Duct Propagation Using Finite Elements;AIAA Journal;1980-05
5. A finite element method for computing sound propagation in ducts containing flow;5th Aeroacoustics Conference;1979-03-12
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