The proposal covers 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 will be supported for achieving a high quality model for a test in cryogenic environment. The tunnel will be 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 will be assessed using temperature sensitive paint. Wing shape will be determined with a stereo camera system. Final data and images are going to be provided to the topic manager. Risk assessment and a dissemination plan are provided.
Fields of science
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