Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap

Author: Tucker, Warren A.
Year: 1944
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-128, NACA-ACR-L4I22
Link: https://digital.library.unt.edu/ark:/67531/metadc61404/

< New search