Measurement of Noise Reduction from Acoustic Casing Treatments Installed Over a Subscale High Bypass Ratio Turbofan Rotor (AIAA 2018-4099)
Aeroacoustics (Conference)
01.01.2018
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust (AIAA 2018-4744)
British Library Conference Proceedings | 2018
|THE NOISE REDUCTION STUDY OF COMPOSITE ACOUSTIC LINER ON HIGH BYPASS RATIO TURBOFAN AEROENGINE
British Library Conference Proceedings | 2021
|DataCite | 1924