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Static longitudinal characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations

Title:Static longitudinal characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations
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Note:National Aeronautics and Space Administration, 1961
  
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Subject:Aerodynamic coefficients
Subject:Aircraft models
Subject:Aspect ratio
Subject:Mach number
Subject:Ptiching moments
Subject:Stability of airplanes, Longitudinal
Subject:Static characteristics
Subject:Subsonic speed
Subject:Wing tips
Subject:Zero lift
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