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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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