Experimental Pressure Distribution on Fuselage Nose and Pilot Canopy of Supersonic Airplane at Mach Number 1.90

Author: Wyatt, DeMarquis D.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E8I07
Link: https://digital.library.unt.edu/ark:/67531/metadc63926/

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