Low-subsonic investigation to determine the chordwise pressure distribution and effectiveness of spoilers on a thin, low-aspect-ratio, unswept, untapered, semispan wing and on the wing with leading and trailing-edge flaps

Author: Croom, Delwin R.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L58B05
Link: https://digital.library.unt.edu/ark:/67531/metadc64128/

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