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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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