The transonic characteristics of 36 symmetrical wings of varying taper, aspect ratio, and thickness as determined by the transonic-bump technique
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Nelson, Warren H↗
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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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Hydrodynamic Tares and Interference Effects for a 12-percent-thick Surface-piercing Strut and an Aspect-ratio-0.25 Lifting Surface
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Ramsen, John A↗
Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds
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Martin, John C↗
Wind-tunnel Investigation at Low Speed of Effect of Size and Position of Closed Air Ducts on Static Longitudinal and Static Lateral Stability Characteristics of Unswept-midwing Models Having Wings of Aspect Ratio 2, 4, and 6
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Jaquet, Byron M↗
Measurements of the Effect of Trailing-edge Thickness on the Zero-lift Drag of Thin Low-aspect-ratio Wings
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Morrow, John D↗
A method for deflection analysis of thin low-aspect-ratio wings
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Stein, Manuel↗
Static Longitudinal and Lateral Stability Characteristics at Low Speed of Unswept-midwing Models Having Wings with an Aspect Ratio of 2, 4, or 6
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Wolhart, Walter D↗
Comparison Between Experimental and Predicted Downwash at a Mach Number of 0.25 Behind a Wing-body Combination Having a Triangular Wing of Aspect Ratio of 2.0
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Sorensen, Norman E↗
Flight Tests at Supersonic Speeds to Determine the Effect of Taper on the Zero-lift Drag of Sweptback Low-aspect-ratio Wings
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Pittel, Murray↗
Analysis of Wind-tunnel Tests to a Mach Number of 0.90 of a Four-engine Propeller-driven Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10
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Edwards, George G↗
The Results of Wind-tunnel Tests to a Mach Number of 0.90 of a Four-engine, Propeller-driven Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10
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Edwards, George G↗
Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing of aspect ratio 4
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Spreemann, Kenneth P↗
Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees
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Lowry, John G↗
Analysis of static aeroelastic behavior of low-aspect-ratio rectangular wings
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Hedgepeth, John M↗
The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. I : Effects of Horizontal-tail Location and Size on the Longitudinal Characteristics
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Tinling, Bruce E↗
The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. II : Lateral and Directional Characteristics
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Savage, Howard F↗
The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3. III : Effects of Trailing-edge Flaps
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Tinling, Bruce E↗
Wind-tunnel Investigation of the Effect of Clipping the Tips of Triangular Wings of Different Thickness, Camber, and Aspect Ratio - Transonic Bump Method
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Emerson, Horace F↗