Low flight speed fan noise from a supersonic inlet
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45012
Reference12 articles.
1. YF-12 inlet suppression of compressor noise - First results
2. 2Bangert L H Feltz E P, Godby L A , and Miller L D Aerodynamic and Acoustic Behavior of a YF 12 Inlet at Static Conditions NASA CR 163106, Jan. 1981
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. Forward Flight Effects on Fan Noise from Supersonic 2-D Inlets;Journal of Aircraft;2006-09
2. Experimental and numerical studies of the aeroacoustics of axisymmetric supersonic inlets;Journal of Sound and Vibration;1995-08
3. Fan Noise Reduction From a Supersonic Inlet During Simulated Aircraft Approach;Journal of Engineering for Gas Turbines and Power;1995-04-01
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