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High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2
Author:
Osborne, Robert S.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9C04
Link:
https://digital.library.unt.edu/ark:/67531/metadc58228/
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