An Investigation of the Subsonic Speed Range of a Full-span and a Semispan Model of a Plane Wing and of a Cambered and Twisted Wing, All Having 45 Degrees of Sweepback
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Shibata, Harry H↗
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Investigation of three tapered 45 degree sweptback cambered and twisted wings covering a simultaneous variation in aspect ratio and thickness ratio and of one related symmetrical wing at transonic speeds by the wing-flow method
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Johnson, Harold I↗
Investigation of the low-speed aerodynamic characteristics of a variable-sweep airplane model with a wing having partial-span cambered-leading-edge modifications
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Becht, Robert E↗
Effects of Twist and Camber, Fences, and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristics of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Foster, Gerald V↗
Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45 degree sweptback wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6) as determined by pressure distributions, force tests
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Pratt, George L↗
A Flight Investigation of the Effect of Leading-edge Camber on the Aerodynamic Characteristics of a Swept-wing Airplane
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Anderson, Seth B↗
A transonic wind-tunnel investigation of the characteristics of a twisted and cambered 45 degree sweptback wing-fuselage configuration
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Harrison, Daniel E↗
Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
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Daley, Bernard N↗
The influence of a change in body shape on the effects of twist and camber as determined by a transonic wind-tunnel investigation of a 45 degree sweptback wing-fuselage configuration
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Harrison, Daniel E↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris
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Hamilton, Clyde V↗
Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6
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Holdaway, George H↗
Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 x 10(exp 6).
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Foster, Gerald V↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the static lateral stability characteris
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Hilton, John H , Jr↗
Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effects of Sweep Angle and Thickness Ratio on the Aerodynamic Characteristics in Pitch
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Driver, Cornelius↗
Investigation of the Low-speed Aerodynamic Characteristics of a Variable-sweep Airplane Model with a Twisted and Cambered Wing
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Becht, Robert E↗
Stability Characteristics at Low Speed of a Variable-sweep Airplane Model Having a Partially Cambered Wing with Several Chord-extension Configurations
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Becht, Robert E↗
A transonic wind-tunnel investigation of the effects of twist and camber with and without incidence, twist and body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body configuration
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Cooper, J Lawrence↗
Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio -transonic bumb method
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Emerson, Horace F↗