Aerodynamic characteristics of NACA RM 10 missile in 8 by 6 foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98. 3: analysis of force distribution at angle of attack (stabilizing fins removed)

Author: Luidens, Roger W.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E50I19
Link: https://digital.library.unt.edu/ark:/67531/metadc58664/

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