Abstract
A separated flow in a truncated ideal contour nozzle due to overexpansion is studied numerically for different pressure ratios. The classical pattern of a FSS is obtained for very low and high pressure ratios. Between these two ranges of pressure ratios, an uncommon cap shock pattern without reattachment of the boundary layer appears. The influence of the thick base annulus height on the separated nozzle flow is also studied. The results are then compared and validated using experimental data. This article was chosen from Selected Proceedings of the 1st French Seminar on Turbulence and Space Launchers (CNES-Paris, 13-14 June 2002) ed P Vuillermoz, P Comte and M Lesieur.
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.
