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Results for “aspect ratio”

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 829 records · Page 46

All sources NASA NTRS DOE OSTI

NASA NTRS1952

The interference effects of a body on the spanwise load distributions of two 45 degrees sweptback wings of aspect ratio 8 from low-speed tests at a Reynolds number of 4 x 10(exp 6)

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Martina, Albert P↗

NASA NTRS1952

Lift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : an Investigation at Large Reynolds Numbers of the Low-speed Characteristics of Several Wing-body Combinations

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Smith, Donald W↗

NASA NTRS1954

The twisting effect at transonic speeds of spoiler ailerons on a 45 degree sweptback, aspect-ratio-4, tapered wing

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Hammond, Alexander D↗

NASA NTRS1954

Low-speed Chordwise Pressure Distributions near the Midspan Station of the Slotted Flap and Aileron of a 1/4-scale Model of the Bell X-1 Airplane with a 4-percent-thick, Aspect-ratio-4, Unswept Wing

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Moseley, William C , Jr↗

NASA NTRS1954

The Transonic Characteristics of Unswept Wings Having Aspect Ratios of 4, Spanwise Variations in Thickness Ratio, and Variations in Plan-Form Taper-Transonic -Bump Technique

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Nelson, Warren H↗

NASA NTRS1954

The effects of horizontal-tail location and size on the subsonic longitudinal aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3

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Tinling, Bruce E↗

NASA NTRS1954

Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness

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Heitmeyer, John C↗

NASA NTRS1954

Comparison of Experimental with Calculated Results for the Lifting Effectiveness of a Flexible 45 Degree Sweptback Wing of Aspect Ratio 6.0 at Mach Numbers from 0.8 to 1.3

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Walters, Richard E↗

NASA NTRS1954

The Effects of Changes in Aspect Ratio and Tail Height on the Longitudinal Stability Characteristics at High Subsonic Speeds of a Model with a Wing Having 32.6 Degree Sweepback

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Alford, William J , Jr↗

NASA NTRS1954

The Transonic Aerodynamic Characteristics of Structurally Related Wings of Low Aspect Ratio Having a Spanwise Variation in Thickness Ratio-transonic Bump Technique

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Cleary, Joseph 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

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↗

NASA NTRS1954

Free-flight Tests of 45 Degree Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds

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O'Kelly, Burke R↗

NASA NTRS1954

Pressure Distributions on Plug-and Semaphore-type Spoiler Ailerons on a 35 Degree Sweptback Wing of Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section at High Subsonic Speeds

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Hammond, Alexander D↗

NASA NTRS1954

A Flight Investigation at Transonic Speeds of the Aerodynamic Characteristics of a Model Having a Thin Unswept Wing of Aspect Ratio 3.1

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White, Maurice D↗

NASA NTRS1954

An experimental investigation of the flutter of several wings of varying aspect ratio, density, and thickness ratio at Mach numbers from 0.60 to 1.10

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Herrera, Raymond↗

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 NTRS1954

The Effects of Operating Propellers on the Longitudinal Characteristics at High Subsonic Speeds of a Four-engine Tractor Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10

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Sutton, Fred B↗