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Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90

Title:Flight evaluation of splitter-plate effectiveness in reducing base drag at Mach numbers from 0.65 to 0.90
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Note:National Aeronautics and Space Administration ;, 1967
  
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Subject:Aerodynamic drag
Subject:Base flow
Subject:Drag reduction
Subject:F-104 aircraft
Subject:Flight tests
Subject:Mach number
Subject:Plates
Subject:Reynolds number
Subject:Subsonic speed
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