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Results for “trailing edge flap”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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At least 127 records · Page 7

All sources NASA NTRS DOE OSTI

NASA NTRS1950

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↗

NASA NTRS1950

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↗

NASA NTRS1950

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↗

NASA NTRS1950

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↗

NASA NTRS1951

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↗

NASA NTRS1951

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↗

NASA NTRS1951

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↗

NASA NTRS1951

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↗

NASA NTRS1951

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↗

NASA NTRS1952

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↗

NASA NTRS1952

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↗

NASA NTRS1953

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↗

NASA NTRS1953

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↗

NASA NTRS1954

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↗

NASA NTRS1954

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↗

NASA NTRS1954

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↗

NASA NTRS1955

Estimation of Incremental Pitching Moments Due to Trailing-Edge Flaps on Swept and Triangular Wings

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James, Harry A↗

NASA NTRS1955

The Effects of Trailing-edge Flaps on the Subsonic Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3

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Tinling, Bruce E↗