Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a 1/15-Scale Model of the Grumman F11F-1F Airplane at Mach Numbers of 1.56, 1.76, 2.06, and 2.53

Author: Turner, Kenneth L.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL56K21
Link: https://digital.library.unt.edu/ark:/67531/metadc53105/

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