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Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel IV : the effect of a constant-chord leading-edge flap at high subsonic speeds
Author:
Reed, Verlin D
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A8K19
Link:
https://digital.library.unt.edu/ark:/67531/metadc58008/
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