Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences

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Wind-tunnel Investigation at Low Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for a Uniform Load at a Lift Coefficient of 0.5

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Wind-tunnel Investigation at L; Ow Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for Uniform Load at a Lift Coefficient of 0.5 and with a Thickened Tip Section

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Wind-tunnel Investigation at Low Speed of the Effects of Chordwise Wing Fences and Horizontal-tail Position on the Static Longitudinal Stability Characteristics of an Airplane Model with a 35 Degree Sweptback Wing

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Low Speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Swept Leading Edge

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Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge

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Wind Tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of a 45 Degree Sweptback-wing-body Combination

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Low Speed Wind Tunnel Investigation of Aerodynamic Characteristics of Swept-back and Swept-forward Wings with a Double Circular-arc Profile

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Subsonic Wind Tunnel Tests on a 40 Degrees Swept-back Wing Fitted with Vortex Generators

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Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Degrees

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