Aerospace Stiffened Panel Analysis Software / Screenshots
 Geometrical dimensions can be specified “on the design” — customary for design engineers.
 Design Manger form is organized as wizard and assists users in specifying necessary source data.
 There is a possibility to specify source data with a high detalization of wing design elements (cross-section and joint type — riveted or integral), ...
 ... crack propagation scenario, and mode of failure.
 Mechanical properties setting includes elastic moduli as well as plasticity characteristics (flow curves).
 Computation starts in batch mode; multisequencing is available in distributed computing environment.
 Results visualization: diagram forms are convenient for the case study.