Effects of turbofan engine intake droop and length on fan tone noise
Author:
Affiliation:
1. University of Southampton
Publisher
American Institute of Aeronautics and Astronautics
Reference14 articles.
1. Response Surface Method Optimization of Uniform and Axially Segmented Duct Acoustics Liners
2. Optimization of Annular and Cylindrical Liners for Mixed Exhaust Aeroengines
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4. 5P. Mustafi, Improved turbofan liner design and optimization. PhD thesis,University of Southampton, 2012.
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