Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 2: presentation and analysis of force measurements

Author: Esenwein, Fred T.
Additional Authors: Obery, Leonard J.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E50D28
Link: https://digital.library.unt.edu/ark:/67531/metadc58428/

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