Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications

Author: Koenig, David G.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56H08
Link: https://digital.library.unt.edu/ark:/67531/metadc62875/

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