The Forces and Pressure Distribution at Subsonic Speeds on a Cambered and Twisted Wing Having 45 Degrees of Sweepback and Aspect Ratio of 3 and a Taper Ratio of 0.5
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Boltz, Frederick W↗
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Results for “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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Lift, Drag and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3 Percent Thick Rounded Nose Section
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Heitmeyer, John C↗
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↗
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Model with Leading-edge Chord-extensions Incorporated on a 40 Degree Sweptback Circular-arc Wing of Aspect Ratio 4 and Taper Ratio 0.50
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Goodson, Kenneth W↗
Tests in the Ames 40- by 80-foot Wind Tunnel of Two Airplane Models Having Aspect Ratio 2 Trapezoidal Wings of Taper Ratios 0.33 and 0.20
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Franks, Ralph W↗
Lift, drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : comparison of three wings of aspect ratio 2 of rectangular, swept-back and triangular plan form, including effects of thickness distribution
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Hightower, Ronald C↗
Transonic wind-tunnel investigation of the effects of aspect ratio, spanwise variations in section thickness ratio, and a body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body combination
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Carmel, Melvin M↗
Effects of a series of inboard plan-form modifications on the longitudinal characteristics of two 47 degree sweptback wings of aspect ratio 3.5, taper ratio 0.2, and different thickness distributions at Mach numbers of 1.61 and 2.01
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Cooper, Morton↗
Transonic Aerodynamic Characteristics in Pitch of a W-wing Having 60 Degree 48 Minute Panel Sweep, Aspect Ratio 3.5, and Taper Ratio 0.25
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Morrison, William D , Jr↗
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↗
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↗
Summary of Some Rocket-model Investigations of Effects of Wing Aspect Ratio and Thickness on Aileron Rolling Effectiveness Including Some Effects of Spanwise Aileron Location for Sweptback Wings with Aspect Ratio of 8.0
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Strass, H Kurt↗
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↗
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↗
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↗
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↗
The effects of circular end plates on the lift, drag, and pitching moment at subsonic and supersonic speeds on a modified triangular wing having an aspect ratio of 2, a taper ratio of 0.33, and a 45 degree swept leading edge
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Peterson, Robert B↗
Effect of Taper Ratio on Lift, Drag, and Pitching-moment Characteristics of Thin Wings of Aspect Ratio 3 with 53.1 Degrees Sweepback of Leading Edge at Subsonic and Supersonic Speeds
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Wetzel, Benton E↗