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Effect of vertical-tail area and length on the yawing stability characteristics of a model having a 45©� sweptback wing

Title:Effect of vertical-tail area and length on the yawing stability characteristics of a model having a 45©� sweptback wing
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Note:National Advisory Committee for Aeronautics, 1951
  
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Subject:Airplanes -- Models -- Testing
Subject:Airplanes -- Tail surfaces
Subject:Airplanes -- Wing, Swept-back
Subject:Stability of airplanes
Subject:Wind tunnel testing
Subject:Yawing (Aerodynamics)
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