Abstract
Models of two/three-position jet noisesuppression nozzles for future supersonic aircraft were acoustically tested under take-off conditions. The tests were conducted simultaneously at the outdoor acoustic facility at CIAM and at the wind-tunnel thrust facility at TSAGI. The mixer-ejector noise-reduction nozzle consists of a multi-lobe two-dimensional nozzle with an acoustically-treated ejector. The influence of the nozzle's basic geometric parameters (number of lobes, shape of lobes, length of ejector) on its noise and thrust performance was investigated. Thrust measurements were made in the external airflow with Mach numbers up to M = 0.6.
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.
