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Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0

Title:Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0
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Note:Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1961., 1961
  
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Subject:Aerodynamics, Supersonic
Subject:Boundary layer control
Subject:Cylinders -- Aerodynamics
Subject:Drag (Aerodynamics)
Subject:Wind tunnels
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