The Online Transonic Small Disturbance flow-solver predicts the transonic flowfield about thin airfoils or through slightly convergent/divergent nozzles by solving the non-linear, transonic small disturbance potential-flow equation. Use the table of contents below to get more information about the use of the site, a very brief introduction to transonic theory to help you understand the results, an outline of the numerical methods utilized, a few references for further reading, and information about the construction and function of the web-site.

Please enjoy the utility, and feel free to pass your questions/comments/complaints on to me. Kevin D. Jones