Print Email Facebook Twitter Business Jet Design Using Laminar Flow Title Business Jet Design Using Laminar Flow Author Boersma, J.Y. Contributor Veldhuis, L.L.M. (mentor) Faculty Aerospace Engineering Department Aerodynamics, Wind Energy & Propulsion Programme Flight Performance & Propulsion Date 2016-11-18 Abstract For conceptual aircraft design to include accurate laminar flow prediction, a link between modern computational tools to determine laminar-to-turbulent boundary layer transition and fast sizing methods is required. For swept wings, it is crucial to include the highly unstable three-dimensional crossflow component of the boundary layer. These topics were connected to judge the impact of laminar flow on business jets, deemed suitable for laminar design considering their relatively low Reynolds number compared to commercial transport. Subject dragN-factorboundary layerskin frictionlaminarflowtransitionReynoldscrossflowaircraftdesignbusinesssweptwinginitiatormodel To reference this document use: http://resolver.tudelft.nl/uuid:4d1818ec-5842-47b0-b144-173aa77a3803 Part of collection Student theses Document type master thesis Rights (c) 2016 Boersma, J.Y. Files PDF Thesis Report J.Y. Boersma.pdf 21.67 MB Close viewer /islandora/object/uuid:4d1818ec-5842-47b0-b144-173aa77a3803/datastream/OBJ/view