Abstract
A pseudo-unsteady system of equations for two-dimensional steady compressible potential flows has been solved by using the rational Runge-Kutta time-stepping procedure combined with the usual central finite difference approximations. Computed results for transonic flows past the NACA 0012 and RAE 2822 airfoils, and subcritical flow around a circular cylinder are compared with the Euler solutions. The potential solution is in close agreement with the Euler one for the case with weak shock waves. For stranger shock waves, significant discrepancy is recognized in the computed flow field due to the entropy production in the Euler solutions.
Sign-in/Register to access full text options 
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 callMore From: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B
Disclaimer: 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.
