Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6

Author: Welsh, Clement J
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55G14
Link: https://digital.library.unt.edu/ark:/67531/metadc61582/

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