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Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel : influence of trailing-edge flap span and deflection on the longitudinal characteristics
Author:
Cancro, Patrick A.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SL54H27
Link:
https://digital.library.unt.edu/ark:/67531/metadc60848/
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