Affiliation:
1. Institut Pprime
2. Instituto Tecnologico de Aeronautica
Publisher
American Institute of Aeronautics and Astronautics
Reference34 articles.
1. Acoustics and Thrust of Quiet Separate-Flow High-Bypass-Ratio Nozzles
2. Huff, D. L. "Noise reduction technologies for turbofan engines," Tech. Rep. NASA/TM-2007-214495, NASA,2007. URLhttps://pdfs.semanticscholar.org/966d/da19dc288d7ae87a4575bf7c1f507081df42.pdf.
3. Aircraft noise reduction technologies: A bibliographic review
4. Fan Noise Reduction: An Overview