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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