Print Email Facebook Twitter Windtunnel investigation with a two-dimensional airfoil on the effect of blowing over a flap and over a control surface Title Windtunnel investigation with a two-dimensional airfoil on the effect of blowing over a flap and over a control surface Author van den Berg, B. Institution National Aerospace Laboratory NLR Date 1962-09-28 Abstract The first part of the investigation deals with blowing over a flap deflected to angles up to 75°. The width of the blowing slot, located in the wing just ahead of the flap, could be varied. Lift, drag and pitching moment have been measured. The results have been compared with those of other similar eiperiments. In the second part the effect of blowing over a control surface with an exposed overhang balance has been investigated. To reference this document use: http://resolver.tudelft.nl/uuid:1a2bef8d-9790-4e64-a5b0-4796428179a9 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 215 Part of collection Aerospace Engineering Reports Document type report Rights (c) 1962 National Aerospace Laboratory NLR Files PDF NLR-MP.215.pdf 33.25 MB Close viewer /islandora/object/uuid:1a2bef8d-9790-4e64-a5b0-4796428179a9/datastream/OBJ/view