Investigation at Mach Number 1.62 of the Pressure Distribution over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap
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Czarnecki, K R↗
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Measurements of Aerodynamic Characteristics of a 35 Degree Sweptback NACA 65-009 Airfoil Model with 1/4-chord Bevelled-trailing-edge Flap and Trim Tab by the NACA Wing-flow Method
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Johnson, Harold I↗
Low-speed investigation of leading-edge and trailing-edge flaps on a 47.5 degree sweptback wing of aspect ratio 3.4 at a Reynolds number of 4.4 x 10(exp 6)
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Pasamanick, Jerome↗
Low-speed longitudinal characteristics of a circular-arc 52 degree sweptback wing of aspect ratio 2.84 with and without leading-edge and trailing-edge flaps at Reynolds numbers from 1.6 x 10(exp 6) to 9.7 x 10(exp 6)
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Foster, Gerald V↗
Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6)
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Salmi, Reino J↗
Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps : Flaps Deflected in Combination
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Stivers, Louis S , Jr↗
Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Leading-edge Flaps Deflected
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Stivers, Louis S , Jr↗
Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
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Stivers, Louis S , Jr↗
Investigation at Supersonic Speeds of Some of the Factors Affecting the Flow over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap
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Czarnecki, K R↗
Effects on Control Effectiveness of Systematically Varying the Size and Location of Trailing-edge Flaps on a 45 Degrees Sweptback Wing at a Mach Number of 1.9
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Jacobsen, Carl R↗
Investigation at Low Speed of the Downwash, Sidewash, and Wake Characteristics Behind a Large-scale Triangular Wing, Including the Effects of Yaw, Full-span Trailing-edge Flaps, and Two Leading- Edge Modifications
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Whittle, Edward F JR↗
Aerodynamic Characteristics of Two 25-percent-area Trailing-edge Flaps on an Aspect Ratio 2 Triangular Wing at Subsonic and Supersonic Speeds
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Boyd, John W↗
The Use of Area Suction for the Purpose of Improving Trailing-edge Flap Effectiveness on a 35 Degree Sweptback Wing
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Holzhauser, Curt A↗
Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
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Dunning, Robert W↗
Effect on the Low-speed Aerodynamic Characteristics of a 49 Degree Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air over the Trailing-edge Flap and Aileron
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Whittle, Edward F , Jr↗
Effects of fences, leading-edge chord extensions, boundary-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60 degree sweptback-wing-indented-body configuration at transonic speeds
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Fischetti, Thomas L↗
The Use of Area Suction to Increase the Effectiveness of a Trailing-edge Flap on a Triangular Wing of Aspect Ratio 2
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Kelly, Mark W↗
Estimation of Incremental Pitching Moments Due to Trailing-Edge Flaps on Swept and Triangular Wings
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James, Harry A↗