Preliminary drag measurements of the consolidated Vultee XF-92A delta-wing airplane in flight tests to a Mach number of 1.01

Author: Bellman, Donald R.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53J23
Link: https://digital.library.unt.edu/ark:/67531/metadc59900/

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