Effects of inflow distortion profiles on fan tone noise calculated using a 3-D theory
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, Ohio; National Aerospace Laboratory, Tokyo, Japan
2. NASA, Lewis Research Center, Turbomachinery Noise Section, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-577
Reference20 articles.
1. Summary of forward velocity effects on fan noise
2. Modal propagation angles in a cylindrical duct with flow and their relation to sound radiation
3. Three-dimensional effects on pure tone fan noise due to inflow distortion
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. Predicted and Observed Modal Radiation Patterns from JT15D Engine with Inlet Rods;Journal of Aircraft;1980-07
2. Comparison of several inflow control devices for flight simulation of fan tone noise using a JT15D-1 engine;6th Aeroacoustics Conference;1980-06-04
3. Analysis of radiation patterns of interaction tones generated by inlet rods in the JT15D engine;5th Aeroacoustics Conference;1979-03-12
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