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Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 /

Title:Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2 /
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Note:Washington, [D.C.] : National Aeronautics and Space Administration, 1961
  
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Subject:Angle of attack
Subject:Aspect ratio
Subject:Transonic wind tunnels
Subject:Aerodynamic characteristics
Subject:Airfoil profiles
Subject:Supersonic speed
Subject:Sweptback wings
Subject:Wing loading
Subject:Wind tunnel tests
Subject:Aerodynamic loads
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