Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000

Author: Salmi, Reino J.
Additional Authors: Conner, D. William
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L7E13
Link: https://digital.library.unt.edu/ark:/67531/metadc64565/

< New search