Print Email Facebook Twitter Vortex flow and Vortex breakdown above delta wing in high subsonic flow Title Vortex flow and Vortex breakdown above delta wing in high subsonic flow Author Donohoe, S.R. Contributor Bakker, P.G. (promotor) Faculty Aerospace Engineering Date 1996-06-14 Subject aerodynamicsdelta wingvortex flowflow visualizationschlierenvortex breakdowntansonic flowwind tunnel testingfive-holve probe To reference this document use: http://resolver.tudelft.nl/uuid:575b510c-8894-4dfb-96d3-521be883580e ISBN 90-5623-036-0 Part of collection Institutional Repository Document type doctoral thesis Rights (c) 1996 S.R. Donohoe Files PDF ae_donohoe_19960614.PDF 13.42 MB Close viewer /islandora/object/uuid:575b510c-8894-4dfb-96d3-521be883580e/datastream/OBJ/view