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Determination of Longitudinal Stability of the Bell X-1 Airplane From Transient Responses at Mach Numbers Up to 1.12 at Lift Coefficients of 0.3 and 0.6
Author:
Angle, Ellwyn E.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L50I06a
Link:
https://digital.library.unt.edu/ark:/67531/metadc58665/
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