Low-Speed Investigation of the Aerodynamic Loads on the Droop-Nose Flap of a Wing With Leading Edge Swept Back 47.5 Degrees and Having Symmetrical Circular-Arc Airfoil Sections at a Reynolds Number of 4.3 X 10 (Exp 6)

Author: Whittle, Edward F., Jr.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9K04
Link: https://digital.library.unt.edu/ark:/67531/metadc58347/

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