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Calculations of the supersonic wave drag of nonlifting wings with arbitrary sweepback and aspect ratio : wings swept behind the Mach lines
Author:
Harmon, Sidney M.
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1319
Link:
https://digital.library.unt.edu/ark:/67531/metadc55502/
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