Wind-Tunnel Investigation at Low Speed of a Wing Swept-Back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5

Author: Weiberg, James A.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A50A23
Link: https://digital.library.unt.edu/ark:/67531/metadc58464/

< New search