Forward flight effects on fan noise from supersonic 2-D inlets
Author:
Affiliation:
1. Florida Agricultural and Mechanical Univ.; Florida State Univ., Tallahassee
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-350
Reference17 articles.
1. YF-12 inlet suppression of compressor noise - First results
2. Trefy, C. J. and Wasserbauer, J. W. "Low-speed Performance of an Axisymmetric, Mixed-compression, Supersonic Inlet with Auxiliary Inlets0022, NASA TP-2557, 1986.
3. Fan Noise Reduction From a Supersonic Inlet During Simulated Aircraft Approach
4. Experimental and numerical studies of the aeroacoustics of axisymmetric supersonic inlets
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