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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration

Title:Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration
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Note:National Aeronautics and Space Administration, 1960
  
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Subject:Aerodynamics
Subject:Airplanes -- Wings, Swept-back
Subject:Mach number
Subject:Short take-off and landing aircraft -- Longitudinal stability
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