A comparison of flight test results on a scout-bomber airplane with 4.7 degree and with 10 degree geometric dihedral in the wing outer panels

Author: Forsyth, Charles M.
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1407
Link: https://digital.library.unt.edu/ark:/67531/metadc55483/

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