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Wind-Tunnel Investigation of the Use of Leading-Edge and Trailing-Edge Area-Suction Flaps on a 13-Percent-Thick Straight Wing and Fuselage Model
Author:
Holzhauser, Curt A.
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A57K01
Link:
https://digital.library.unt.edu/ark:/67531/metadc63996/
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