Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 employing high-velocity blowing over the leading- and trailing-edge flaps

Author: Hickey, David H.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A58A09
Link: https://digital.library.unt.edu/ark:/67531/metadc63718/

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