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Investigation at mach numbers of 0.60 to 3.50 of blended wing-body combinations with cambered and twisted wings with diamond, delta and arrow plan forms

Title:Investigation at mach numbers of 0.60 to 3.50 of blended wing-body combinations with cambered and twisted wings with diamond, delta and arrow plan forms
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Note:National Aeronautics and Space Administration, 1961
  
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Subject:Aerodynamics -- Testing
Subject:Airplanes -- Control surfaces -- Testing
Subject:Airplanes -- Wings -- Testing
Subject:Drag (Aerodynamics)
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