Pressure-distribution investigation of an NACA 0009 airfoil with an 80-percent-chord plain flap and three tabs

Author: Ames, Milton B., Jr.
Year: 1940
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-761
Link: https://digital.library.unt.edu/ark:/67531/metadc54636/

< New search