Impact of Future Low-Emissions Combustor Technology on Acoustic Scaling Laws

Author:

McCormick Duane C.1,Hultgren Lennart S.2,Mendoza Jeffrey M.1

Affiliation:

1. Raytheon Technologies Research Center

2. NASA John H Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Berton, J. J., Envia, E., and Burley, C. L. "An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal,"AIAAPaper2009-3144,16thAIAA/CEASAerocousticsConference,Miami,Florida,2009. doi:10.2514/6.2009-3144.

2. Smith, L. L. "Fuel Flexible Combustor for High-OPR Compact-Core N+3 Propulsion Engine," Contractor Report NASA/CR2020-220498,NASA,2020. URL https://ntrs.nasa.gov/citations/20200001621.

3. McCormick, D., Snyder, J., Kim, W., and Mendoza, J. M. "Acoustics of Future Low-Emissions Combustor Technology, Volume 1: Final Report," Contractor Report NASA/CR-20205011099/VOL1, NASA,2020. URLhttps://ntrs.nasa.gov/ citations/20205011099.

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