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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