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Effect of area-suction-type boundary-layer control on the landing-approach characteristics of a 35 degree swept-wing fighter
Author:
Cooper, George E
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A55K14
Link:
https://digital.library.unt.edu/ark:/67531/metadc61835/
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