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A Transonic Investigation by the Free-Fall Method of an Airplane Configuration Having 45 Degrees Sweptback Wing and Tail Surfaces
Author:
Faber, Stanley
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53D10
Link:
https://digital.library.unt.edu/ark:/67531/metadc59799/
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