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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