The Effect of Sweepback on the Longitudinal Characteristics at a Mach Number of 1.24 of a 1/30 Scale Semispan Model of the Bell X-5 Airplane From Tests by the NACA Wing Flow Method

Author: Morris, Garland J.
Additional Authors: Kennedy, Robert M.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50I28
Link: https://digital.library.unt.edu/ark:/67531/metadc58683/

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