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Comparison of Wind-Tunnel, Rocket, and Flight Drag Measurements for Eight Airplane Configurations at Mach Numbers Between 0.7 and 1.6
Author:
Purser, Paul E.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54F18
Link:
https://digital.library.unt.edu/ark:/67531/metadc60570/
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