Small-scale transonic investigation of the effects of twist and camber on the aerodynamic characteristics of a 60 degrees 42' sweptback wing of aspect ratio 1.94

Author: Spreemann, Kenneth P.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51I21
Link: https://digital.library.unt.edu/ark:/67531/metadc59044/

< New search