Longitudinal stability and control characteristics of a semispan airplane model at transonic speeds as obtained by the transonic-bump method

Author: Weil, Joseph
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8B03
Link: https://digital.library.unt.edu/ark:/67531/metadc57960/

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