A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

Author: Danforth, Edward C. B.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51G20
Link: https://digital.library.unt.edu/ark:/67531/metadc58849/

< New search