Print Email Facebook Twitter Analysis of experimental data for a 21% thick natural laminar flow airfoil, NAE 68-060-21:1 Title Analysis of experimental data for a 21% thick natural laminar flow airfoil, NAE 68-060-21:1 Author Jones, D.J. Khalid, M. Institution National Research Council Canada, National Aeronautical Establishment Date 1985-10-30 Abstract NAE and de Havilland Aircraft of Canada have designed and tested in the NAE 5 ft X 5 ft wind tunnel a 21% thick supercritical airfoil capable of sustaining long runs of laminar flow on both surfaces. The measured drag levels are superior to those of any model previously tested in this facility and are comparabIe to classical NACA and modern NASA NLF airfoils. To reference this document use: http://resolver.tudelft.nl/uuid:cbc58e17-bf80-41ae-93cf-578764550608 Publisher National Research Council Canada Access restriction Campus only Source National Aeronautical Establishment, Aeronautical Note NAE-AN-34, NRC no 25076 Part of collection Aerospace Engineering Reports Document type report Rights (c) 1985 National Research Council Canada Files PDF NAE-AN-34.pdf 7.78 MB Close viewer /islandora/object/uuid:cbc58e17-bf80-41ae-93cf-578764550608/datastream/OBJ/view