Mach (top) and pressure (bottom) contours for axisymmetric Busemann inlet with evenly spaced bleed perforations along length of inlet. Images show changes in Mach and pressure contours as a function of inlet length ranging from inlet start (left) and inlet throat (right). Contours were produced via Cart 3D, an inviscid code for automated CFD.
The AIAA Dayton-Cincinnati Aerospace Sciences Symposium is a unique venue for technical interchange with members of the regional aerospace community. The event is organized and sponsored by the Executive Council of the AIAA Dayton-Cincinnati Section, and co-sponsored by several local organizations.