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Calculation of the supersonic pressure distribution on a single-curved tapered wing in regions not influenced by the root or tip
Author:
Vincenti, Walter G
Year:
1955
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3499
Link:
https://digital.library.unt.edu/ark:/67531/metadc57922/
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