Results of Preliminary Flight Tests of the XS-1 Airplane (8-Percent Wing) to a Mach Number of 1.25

Author: Williams, W. C.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8A23a
Link: https://digital.library.unt.edu/ark:/67531/metadc57662/

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