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Pressure distribution over a sharp-nose body of revolution at transonic speeds by the NACA wing-flow method
Author:
Danforth, Edward C. B.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L7K12
Link:
https://digital.library.unt.edu/ark:/67531/metadc58141/
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