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Results for “edge effects”

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 361 records · Page 20

All sources NASA NTRS DOE OSTI

NASA NTRS1953

The Effects of Leading-edge Extensions, a Trailing-edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-fuselage-tail Combination Having a Wing with 35 Degrees of Sweepback and an Aspect Ratio of 4.5

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Selan, Ralph↗

NASA NTRS1953

Effects of Leading-edge Slats on the Aerodynamic Characteristics of a 45 Degree Sweepback Wing-fuselage Configuration at Mach Numbers of 0.4 to 1.03

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Runckel, Jack F↗

NASA NTRS1953

Effects of Trailing-edge Bluntness on the Lift, Drag, and Pitching-moment Characteristics of Unswept, 45 Degree Swept, and 45 Degree Delta Wings at Mach Numbers of 1.41, 1.62, and 1.96

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Goin, Kennith L↗

NASA NTRS1954

Effects of Leading-edge Chord Extensions and an All-movable Horizontal Tail on the Aerodynamic Characteristics of a Wing-body Combination Employing a Triangular Wing of Aspect Ratio 3 Mounted in a High Position at Subsonic and Supersonic Speeds

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Wetzel, Benton E↗

NASA NTRS1955

Experimental investigation at high subsonic speeds of the effects of leading-edge radius on the aerodynamic characteristics of a sweptback-wing - fuselage combination with leading-edge flaps and chord-extensions

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Spreemann, Kenneth P↗

NASA NTRS1955

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

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Foster, Gerald V↗

NASA NTRS1955

Drag and Rolling-moment Effectiveness of Trailing-edge Spoilers at Mach Numbers 2.2 and 5.0

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Canning, Thomas N↗

NASA NTRS1955

The Effect of Leading-edge Droop upon the Pressure Distribution and Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at Transonic Speeds

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Schmeer, James W↗

NASA NTRS1956

The Effect of Leading-edge Extensions on the Longitudinal Characteristics at Mach Numbers up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution

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Sutton, Fred B↗

NASA NTRS1955

Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

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Wetzel, Benton E↗

NASA NTRS1955

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by Reynolds numbers up to 8.00 x 10(exp 6) and Mach numbers up to 0.29

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Foster, Gerald V↗

NASA NTRS1956

The Effect of Trailing-edge Bluntness on the Performance of a Small-scale Supersonic Propeller at Forward Mach Numbers to 0.92

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Demele, Fred A↗

NASA NTRS1955

A Systematic Study of the Effects of Leading-edge Chord-extensions on the Low-speed Longitudinal Stability Characteristics of Three 45 Degree Sweptback Wings

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Kelly, H Neale↗

NASA NTRS1956

Effect of Leading-edge Droop on the Aerodynamic and Loading Characteristics of a 4-percent-thick Unswept-wing--fuselage Combination at Transonic Speeds

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Schmeer, James W↗

NASA NTRS1955

The Effects of Trailing-edge Flaps on the Subsonic Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3

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Tinling, Bruce E↗

NASA NTRS1956

Investigation of the Use of Area Suction to Increase the Effectiveness of Trailing-edge Flaps of Various Spans on a Wing of 45 Degree Sweepback and Aspect Ratio 6

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Griffin, Roy N , Jr↗

NASA NTRS1956

Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers

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Schneider, William C↗

NASA NTRS1958

Flight evaluation of the effects of leading-edge-slat span on the stability and control characteristics of a swept-wing fighter-type airplane during accelerated longitudinal maneuvers at transonic speeds

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Matranga, Gene J↗