Abstract
Recently, a singular integral method was developed for solving two-dimensional compressible potential flows. The original formulation limited the applicability to single bodies in a uniform freestream. Currently, modifications are being made so that the flow field around multiple bodies can also be calculated. Because of the unique manner in which the integral equations are formulated, they are especially well-suited for analysis and inverse design calculations of a row of similar airfoils. A brief description of the formulation is given in this paper and some preliminary results are included.
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.
