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The calculation of drag for airfoil sections and bodies of revolution at subcritical speeds
Author:
Heaslet, Max A
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A7B06
Link:
https://digital.library.unt.edu/ark:/67531/metadc58035/
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