Abstract
NASA and the General Electric Co. are jointly developing two low noise propulsion technology demonstrators (Engine A and C incorporating, respectively, a low tip speed and high tip speed fan) under the Experimental Quiet Engine Program. The acoustic and Aerodynamic performance characteristics of Engine C which is currently on test will be reported at a later date. The present paper describes the design, component development and engine evaluation of the A demonstrator. The aerodynamic and acoustic performance obtained on the fan component are discussed. The demonstrator engine acoustic test program is outlined. The effect of inlet geometry and duct acoustic treatment are presented. The static acoustic data are extrapolated to flight and compared with the FAA noise regulations.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
