Investigation of NACA 65(sub 112) A111 (approx.) airfoil with 0.35-chord slotted flap at Reynolds numbers up to 25 million

Author: Racisz, Stanley F.
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1463
Link: https://digital.library.unt.edu/ark:/67531/metadc54268/

< New search