Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections

Author: Anderson, Raymond F.
Year: 1934
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-487
Link: https://digital.library.unt.edu/ark:/67531/metadc54379/

< New search