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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 ...

The primary innovative approach and the major aim of the investigations being covered here is in the first instance to perform reliable and high quality procedures for laminar wing testing under and near flight conditions at high Reynolds numbers in ETW. Beside confirming a number of already mature and successfully applied measuring techniques, these investigations will allow to validate a new eva ...