Flight measurements of the longitudinal stability, stalling, and lift characteristics of an airplane having a 35 degrees sweptback wing without slots and with 40-percent-span slots and a comparison with wind-tunnel data

Author: Sjoberg, S. A.
Year: 1948
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1679
Link: https://digital.library.unt.edu/ark:/67531/metadc54759/

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