Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effects of Split Flaps, Elevons, and Leading-edge Devices at Low Speed
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Hopkins, Edward J↗
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Results for “flaps”
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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Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 45 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section
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Vogler, Raymond D↗
Investigation at large scale of the pressure distribution and flow phenomena over a wing with the leading edge swept back 47.5 degrees having circular-arc airfoil sections and equipped with drooped-nose and plain flaps
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Lange, Roy H↗
Investigation at Mach Number 1.62 of the Pressure Distribution over a Rectangular Wing with Symmetrical Circular-arc Section and 30-percent-chord Trailing-edge Flap
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Czarnecki, K R↗
Low-speed investigation of the aerodynamic loads on the droop-nose flap of a wing with leading edge swept back 47.5 degrees and having symmetrical circular-arc airfoil sections at a Reynolds number of 4.3 x 10 (exp 6)
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Whittle, Edward F , Jr↗
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↗
Exploratory Investigation of the Effect of Skewed Plain Nose Flaps on the Low-speed Characteristics of a Large-scale Triangular-wing-fuselage Model
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Wick, Bradford H↗
Lateral-control investigation of flap-type controls on a wing with upswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method
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Hammond, Alexander D↗
Full-scale Investigation of Boundary-layer Control by Suction Through Leading-edge Slots on a Wing-fuselage Configuration Having 47.5 Degree Leading-edge Sweep with and Without Flaps
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Pasamanick, Jerome↗
Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic bump method
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Vogler, Raymond D↗
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↗
Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method
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Thompson, Robert F↗
Effects of Varying the Size and Location of Trailing-edge Flap-type Controls on the Aerodynamic Characteristics of a Unswept Wing at a Mach Number of 1.9
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Mitchell, Meade H , Jr↗
Lateral-control investigation of flap-type and spoiler-type controls on a wing with quarter-chord-line sweepback of 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method
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Hammond, Alexander D↗
The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
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Rathert, George A , Jr↗
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↗
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↗
The Time Lag Between Flap Deflection and Force Development at a Mach Number of 4
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Lindsey, Walter F↗