Force and Moment Coefficients for a Thin Airfoil With Flap and Tab in a Form Useful for Stability and Control Calculations

Author: White, Roland J.
Year: 1945
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-960
Link: https://digital.library.unt.edu/ark:/67531/metadc54927/

< New search