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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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At least 577 records · Page 32

All sources NASA NTRS DOE OSTI

NASA NTRS1956

The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-engine Tractor Airplane Configuration Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10

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Lopez, Armendo E↗

NASA NTRS1958

Analytical and experimental investigation of aerodynamic forces and moments on low-aspect-ratio wings undergoing flapping oscillations

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Woolston, Donald S↗

NASA NTRS1958

Static longitudinal and lateral stability characteristics at low speed of 60 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6

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Wolhart, Walter D↗

NASA NTRS1958

Some measurements of aerodynamic forces and moments at subsonic speeds on a rectangular wing of aspect ratio 2 oscillating about the midchord

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Widmayer, Edward, Jr↗

NASA NTRS1958

Flutter analysis of rectangular wings of very low aspect ratio

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Fralich, Robert W↗

NASA NTRS1958

The Effects of an Inverse-taper Leading-edge Flap on the Aerodynamic Characteristics in Pitch of a Wing-body Combination Having an Aspect Ratio of 3 to 45 Degrees of Sweepback at Mach Numbers to 0.92

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Demele, Fred A↗

NASA NTRS1958

Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Aspect-ratio-10 Wing, Two Propellers, and Area-suction Flaps

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Weiberg, James A↗

NASA NTRS1948

An investigation of the downwash behind a high-aspect-ratio wing with various amounts of sweep in the Langley 8-foot high-speed tunnel

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Whitcomb, Richard T↗

NASA NTRS1948

Langley Full-scale Tunnel Investigation of the Characteristics in Yaw of a Trapezoidal Wing of Aspect Ratio 4 with Circular-arc Airfoil Sections

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Stevens, George L↗

NASA NTRS1948

Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel I : Characteristics of a Plain Wing

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Johnson, Ben H , Jr↗

NASA NTRS1948

Low-speed investigation of a small triangular wing of aspect ratio 2.0 III : static stability with twin vertical fins

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Rose, Leonard↗

NASA NTRS1948

Effect of Leading-edge High-lift Devices and Split Flaps on the Maximum-lift and Lateral Characteristics of a Rectangular Wing of Aspect Ratio 3.4 with Circular-arc Airfoil Sections at Reynolds Numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).

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Lange, Roy H↗

NASA NTRS1948

Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel II : The Effect of Constant-chord Leading- and Trailing-edge Flaps on the Low-speed Characteristics of the Wing

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Bandettini, Angelo↗

NASA NTRS1948

Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel II : the Effectiveness and Hinge Moments of a Constant-chord Plain Flap

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Stephenson, Jack D↗

NASA NTRS1948

Static Longitudinal Aerodynamic Characteristics of a 52 Degree Sweptback Wing of Aspect Ratio 2.88 at Reynolds Numbers from 2,000,000 to 11,000,000

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Fitzpatrick, James E↗

NASA NTRS1948

Investigation of Wing Characteristics at a Mach Number of 1.53 III : Unswept Wings of Differing Aspect Ratio and Taper Ratio

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Nielsen, Jack N↗

NASA NTRS1948

Wind-tunnel Investigation of Horizontal Tails IV : Unswept Plan Form of Aspect Ratio 2 and a Two-dimensional Model

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Dods, Jules B , Jr↗

NASA NTRS1948

Effects of aspect ratio on air flow at high subsonic Mach numbers

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Lindsey, W F↗