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Accession Number N20120013872
Title Comparison of Combustor-Noise Models.
Publication Date Jun 2012
Media Count 33p
Personal Author L. S. Hultgren
Abstract The current status of combustor-noise prediction in the NASA Aircraft Noise Prediction Program (ANOPP) for current-generation (N) turbofan engines is summarized. Best methods for near-term updates are reviewed. Long-term needs and challenges for the N+1 through N+3 timeframe are discussed. This work was carried out under the NASA Fundamental Aeronautics Program, Subsonic Fixed Wing Project, Quiet Aircraft Subproject.
Keywords Aeroacoustics
Aircraft configurations
Combustion chambers
Fixed wings
Noise prediction
Turbofan engines

 
Source Agency National Aeronautics and Space Administration
NTIS Subject Category 46A - Acoustics
51C - Aircraft
81D - Jet & Gas Turbine Engines
Corporate Author National Aeronautics and Space Administration, Cleveland, OH. NASA John H. Glenn Research Center at Lewis Field.
Document Type Technical report
Title Note N/A
NTIS Issue Number 1305
Contract Number N/A

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