Drag Characteristics of Rectangular and Swept-back NACA 65-009 Airfoils Having Various Aspect Ratios as Determined by Flight Tests at Supersonic Speeds
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Tucker, Warren A↗
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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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An Investigation of the Lateral-control Characteristics of Spoilers on a High-aspect-ratio Wing of NACA 65-210 Section in the Langley 8-foot High Speed Tunnel
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Luoma, Arvo A↗
An investigation of a high-aspect-ratio wing having 0.20-chord plain ailerons in the Langley 8-foot high-speed tunnel
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Luoma, Arvo A↗
Drag Measurements of a 34 Degree Swept-forward and Swept-back NACA 65-009 Airfoil of Aspect Ratio 2.7 as Determined by Flight Tests at Supersonic Speeds
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Alexander, Sidney R↗
Aerodynamic Characteristics of a 45 Degree Swept-back Wing with Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
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Proterra, Anthony J↗
Effects of Combinations of Aspect Ratio and Sweepback at High Subsonic Mach Numbers
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Adler, Alfred A↗
An Investigation of the Downwash at the Probable Tail Location Behind a High-aspect-ratio Wing in the Langley 8-foot High-speed Tunnel
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Whitcomb, Richard T↗
Drag Measurements of Symmetrical Circular-arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
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Alexander, Sidney R↗
An Investigation at Low Speed of a Large-scale Triangular Wing of Aspect Ratio Two II : the Effect of Airfoil Section Modifications and the Determination of the Wake Downwash
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Anderson, Adrien E↗
Drag Characteristics of Rectangular and Swept-back NACA 65-009 Airfoils Having Aspect Ratios of 1.5 and 2.7 as Determined by Flight Tests at Supersonic Speeds
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Alexander, Sidney R↗
Investigation of Wing Characteristics at a Mach Number of 1.53 I : Triangular Wings of Aspect Ratio 2
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Vincenti, Walter G↗
An investigation of the hinge-moment fluctuations of 0.20-chord plain ailerons on a high-aspect-ratio wing in the Langley 8-foot high-speed tunnel
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Luoma, Arvo A↗
Low-speed Investigation of a Small Triangular Wing of Aspect Ratio 2.0 I : the Effect of Combination with a Body Revolution and Height Above a Ground Plane
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Rose, Leonard M↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected
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Edwards, George G↗
Wing-flow Tests of a Triangular Wing of Aspect Ratio Two I : Effectiveness of Several Types of Trailing-edge Flaps on Flat-plate Models
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FLAPS - COMPLETE WINGS↗
Wind-tunnel Investigation of Horizontal Tails I : Unswept and 35 Degrees Swept-back Plan Forms of Aspect Ratio 3
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Dods, Jules B , Jr↗
Additional Results in a Free-flight Investigation of Control Effectiveness of Full-span, 0.2-chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickne
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Sandahl, Carl A↗
Wind-tunnel Investigation of Horizontal Tails V : 45 Degree Swept-back Plan Form of Aspect Ratio 2
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Dods, Jules B JR↗