HISSS® (Higher-Order Subsonic/Supersonic Singularity Method) is a potential flow solver with subsonic and supersonic capabilities.
At the Institut für Flugzeugbau und Leichtbau HISSS® is manly used do determine aerodynamic performance data and loads for the preliminary design environement PrADO.
Institute of Aircraft Design and Lightweight Structures
Hermann-Blenk-Straße 35
D-38108 Braunschweig
E-Mail: ifl@tu-braunschweig.de
Telephone: +49 531 391 9903