The proposal covered the preparation and performance of a wind tunnel test using an innovative Bizjet with natural laminar flow wings, RC-controlled HTP and nacelles.

Model design, manufacturing and instrumentation were supported for achieving a high-quality model for a test in cryogenic environment. The tunnel was instrumented for performance tests on a z-sting mounted full model acquiring forces, moments as well as steady and unsteady pressure data. Transition location on the wings were assessed using temperature sensitive paint. Wing shape was determined with a stereo camera system.

Final data and images were going to be provided to the topic manager. Risk assessment and a dissemination plan were provided.