Print Email Facebook Twitter Investigation of the unsteady flow over a wing under gust excitation Title Investigation of the unsteady flow over a wing under gust excitation Author Lancelot, P.M.G.J. (TU Delft Aerospace Structures & Computational Mechanics) Sodja, J. (TU Delft Aerospace Structures & Computational Mechanics) De Breuker, R. (TU Delft Aerospace Structures & Computational Mechanics) Date 2017-01-01 Abstract A detailed performance investigation of the gust generator built for the Open Jet Facility wind tunnel at TU Delft is summarised in this paper. The influence of various parameters such as reduced frequency, measurement location, and excitation amplitude on the generated gust profile was quantified. In addition, unsteady lift measurements were performed using a rigid wing exposed to various gust profiles. In addition, unsteady incremental lift was compared with the DLM method which showed good agreement. Subject Gust generatorUnsteady aerodynamicsUnsteady loads To reference this document use: http://resolver.tudelft.nl/uuid:2caf1e73-3de2-4067-803d-8a52c9050fea Publisher International Forum on Aeroelasticity and Structural Dynamics (IFASD) ISBN 9788897576280 Source 17th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2017, 2017-June Event 17th International Forum on Aeroelasticity and Structural Dynamics, 2017-06-25 → 2017-06-28, Como, Italy Part of collection Institutional Repository Document type conference paper Rights © 2017 P.M.G.J. Lancelot, J. Sodja, R. De Breuker Files PDF Investigationoftheunstead ... ion_RG.pdf 1.55 MB Close viewer /islandora/object/uuid:2caf1e73-3de2-4067-803d-8a52c9050fea/datastream/OBJ/view