А.А. Mirzoyan

DoI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_43401176

Optimization of thrust management (TM) at initial climb may give an important reserve to improve noise performance of Supersonic Business Jet (SSBJ). A variable engine nozzle with a variable throat and exhaust area is often used as a component of supersonic propulsion system. Optimization of nozzle throat variation for jet noise reduction may significantly increase the environmental friendliness of SSBJ. Such optimal (low noise) variation of nozzle throat area at engine throttling provides fixed air flow and corresponding additional reduction of engine exhaust jet velocity.

Read the full paper >

In Categories: High-Speed Missions and Vehicles, HiSST 2018, Noise reduction technolgies, Operations and Environment
Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.