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Effect of Reflex Camber on the Aerodynamic Characteristics of a Highly Tapered Moderately Swept-Back Wing at Reynolds Numbers Up to 8,000,000
Author:
Conner, D. William
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1212
Link:
https://digital.library.unt.edu/ark:/67531/metadc55338/
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