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Effects on control effectiveness of systematically varying the size and location of trailing-edge flaps on a 45 degrees sweptback wing at a Mach number of 1.9
Author:
Jacobsen, Carl R.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51I26
Link:
https://digital.library.unt.edu/ark:/67531/metadc59059/
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