A theoretical model of fuselage pressure levels due to fan tones radiated from the intake of an installed turbofan aero-engine
Crossref DOI link: https://doi.org/10.1121/1.5038263
Published Online: 2018-06-07
Published Print: 2018-06-01
Update policy: https://doi.org/10.1063/aip-crossmark-policy-page
Gaffney, James
McAlpine, Alan
Kingan, Michael J.
Funding for this research was provided by:
Engineering and Physical Sciences Research Council
Rolls-Royce