Print Email Facebook Twitter Design and Experimental Validation of Swirl Recovery Vanes for Propeller Propulsion Systems Title Design and Experimental Validation of Swirl Recovery Vanes for Propeller Propulsion Systems Author Li, Q. (TU Delft Flight Performance and Propulsion) Öztürk, K. (TU Delft Aerospace Engineering) Ragni, D. (TU Delft Wind Energy) Sinnige, T. (TU Delft Flight Performance and Propulsion) Eitelberg, G. (TU Delft Flight Performance and Propulsion) Veldhuis, L.L.M. (TU Delft Flight Performance and Propulsion) Yangang, Wang (Northwestern Polytechnical University) Faculty Aerospace Engineering Date 2017 To reference this document use: http://resolver.tudelft.nl/uuid:b3f21d10-cf4c-4dfb-ba23-034071314e38 DOI https://doi.org/10.2514/6.2017-3571 Publisher American Institute of Aeronautics and Astronautics Inc. (AIAA) Embargo date 2018-06-09 ISBN 978-1-62410-501-2 Source 35th AIAA Applied Aerodynamics Conference: 5-9 June 2017, Denver, Colorado Event 35th AIAA Applied Aerodynamics Conference, 2017-06-05 → 2017-06-09, Denver, United States Part of collection Institutional Repository Document type conference paper Rights © 2017 Q. Li, K. Öztürk, D. Ragni, T. Sinnige, G. Eitelberg, L.L.M. Veldhuis, Wang Yangang Files PDF 2017_AIAA_conference_paper.pdf 1.58 MB Close viewer /islandora/object/uuid:b3f21d10-cf4c-4dfb-ba23-034071314e38/datastream/OBJ/view