Jimmy-John HOSTE, Bruno PIAZZA, Fernando MIRO-MIRO

DOI Number XXX-YYY-ZZZ

Conference number: HiSST-2024-0025

In the context of supersonic propulsion the intake plays a crucial role, providing the necessary compression and flow quality to the engine. CFD has become an affordable tool to leverage in such intake design but in order to do so it requires extensive validation. To this end, two supersonic intakes documented in the literature have been numerically studied with the commercial software Simcenter STAR-CCM+. The experience in this endeavour is herein reported. —- For now no extra relevant information to add in here as it will depend on the more in-depth analysis and the results that we’ll get.

In Categories: 1.Events, HiSST 2024, Propulsion Systems and Components
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.