Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 1: presentation and analysis of pressure measurements (stabilizing fins removed)

Author: Luidens, Roger W.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E50D10
Link: https://digital.library.unt.edu/ark:/67531/metadc58512/

< New search