Abstract
In this paper a numerical method for supersonic conical flow without axial symmetry was developed as follows: the governing equations for conical flow without axial symmetry were derived from a pair of stream functions of conical flow and a vorticity equation, and were transformed into Stocker & Mauger's coordinate system. By this method the numerical solutions were also presented for the supersonic flow past conical bodies which produced elliptic conical, nearly conical, and pseudo-triangular conical shock waves, and were compared with other investigator's solutions.
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.
