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Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45©� sweptback wing of aspect ratio 4

Title:Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers of 0.40 to 0.93 of a 45©� sweptback wing of aspect ratio 4
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Note:National Advisory Committee for Aeronautics, 1957
  
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Subject:Airplanes -- Fuselage
Subject:Airplanes -- Wings, Swept-back
Subject:Drag (Aerodynamics)
Subject:Flaps (Airplanes)
Subject:Leading edge flaps
Subject:Leading edges (Aerodynamics)
Subject:Lift (Aerodynamics)
Subject:Pitching (Aerodynamics)
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