Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, a=1.0 Airfoil Section

Author: Quinn, John H., Jr.
Year: 1945
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-82, NACA-CB-L5J04
Link: https://digital.library.unt.edu/ark:/67531/metadc61407/

< New search