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Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4

Title:Investigation of drag reduction by boundary layer suction on a 50-deg swept tapered wing at M (free-stream) = 2.5 to 4
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Note:Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964
  
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Subject:Airplanes -- Wings, Swept-back
Subject:Drag (Aerodynamics)
Subject:Laminar boundary layer
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