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Lift and drag characteristics of the Douglas X-3 research airplane obtained during demonstration flights to a Mach number of 1.20
Author:
Bellman, Donald R
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H54I17
Link:
https://digital.library.unt.edu/ark:/67531/metadc60988/
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