Longitudinal Stability and Control Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds From Tests by the NACA Wing-Flow Method

Author: Silsby, Norman S.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8G30
Link: https://digital.library.unt.edu/ark:/67531/metadc57937/

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