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Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Title:Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
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Note:National Advisory Committee for Aeronautics, 1949
  
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Subject:Aerodynamics, Supersonic
Subject:Airplanes -- Models -- Testing
Subject:Airplanes -- Models -- Wings
Subject:Airplanes -- Wings, Triangular
Subject:Charts, diagrams, etc.
Subject:Leading edges (Aerodynamics)
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