The effects on the aerodynamic characteristics of varying the wing thickness ratio of a triangular wing-body configuration at transonic speeds from tests by the NACA wing-flow method

Author: Hall, Albert W.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52B18
Link: https://digital.library.unt.edu/ark:/67531/metadc59166/

< New search