skip to content
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