Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 and 5.05

Author: Gloria, Hermilo R.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A55K07
Link: https://digital.library.unt.edu/ark:/67531/metadc61900/

< New search