Table of Contents
Loftin, Laurence K, Jr; Bursnall, William J. The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections (Langley Research Center, 1950).
Includes theory and profiles for NACA 4, 5, 6 digit series airfoils
Report number: NACA-TR-964 (Accessible via NASA Technical Reports)
Sources for research articles from journals and conference proceedings.