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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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