Print Email Facebook Twitter Low speed aerodynamic characteristics of an 18% thick airfoil section designed for the all-flying tailplane of the M-300 sailplane Title Low speed aerodynamic characteristics of an 18% thick airfoil section designed for the all-flying tailplane of the M-300 sailplane Author Boermans, L.M.M. Blom, J.J.H. Faculty Aerospace Engineering Date 1976 To reference this document use: http://resolver.tudelft.nl/uuid:d5fdfbbd-9d95-41ea-82bf-1c25fef68aa7 Publisher Delft University of Technology Source Delft University of Technology, Department of Aerospace Engineering, Report LR-226 Part of collection Institutional Repository Document type report Rights (c) 1976 Delft University of Technology Files PDF VTH-226.pdf 1.74 MB Close viewer /islandora/object/uuid:d5fdfbbd-9d95-41ea-82bf-1c25fef68aa7/datastream/OBJ/view