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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 667 records · Page 37

All sources NASA NTRS DOE OSTI

NASA NTRS1950

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↗

NASA NTRS1950

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↗

NASA NTRS1950

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↗

NASA NTRS1950

Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2

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Luoma, Arvo A↗

NASA NTRS1950

Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 45 Degrees, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A009 Airfoil Section

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Spreemann, Kenneth P↗

NASA NTRS1950

A Transonic-wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-fuselage Configuration with a Wing of 45 Degrees Sweepback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfo

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Osborne, Robert S↗

NASA NTRS1950

Wing-flow Measurements of Longitudinal Stability and Control Characteristics of a Supersonic Airplane Configuration Having a 42.8 Degree Sweptback Circular Arc Wing with Aspect Ratio 4.0, Taper Ratio 0.50, and Sweptback Tail Surfaces

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Crane, Harold L↗

NASA NTRS1950

Investigation at transonic speeds of a 35-percent-chord aileron on a tapered wedge-type wing of aspect ratio 2.5 with and without a fuselage

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Turner, Thomas R↗

NASA NTRS1950

The damping in roll of rocket-powered test vehicles having rectangular wings with NACA 65-006 and symmetrical double-wedge airfoil sections of aspect ratio 4.5

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Dietz, Albert E↗

NASA NTRS1950

Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees

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Kemp, William B , Jr↗

NASA NTRS1950

Wind-tunnel Investigation of the Low-speed Longitudinal and Lateral Control Characteristics of a Triangular-wing Model of Aspect Ratio 2.31 Having Constant-chord Control Surfaces

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Wolhart, Walter D↗

NASA NTRS1950

Low-speed Investigation of Deflectable Wing-tip Elevators on a Low-aspect-ratio Untapered 45 Degree Sweptback Semispan Wing with and Without an End Plate

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Fischel, Jack↗

NASA NTRS1950

Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

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Turner, Thomas R↗

NASA NTRS1950

Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section : transonic-bump method

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Macleod, Richard G↗

NASA NTRS1950

Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane

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Heinle, Donovan R↗

NASA NTRS1950

Effect of an End Plate on the Aerodynamic Characteristics of a 20.55 Degree Sweptback Wing with an Aspect Ratio of 2.67 and a Taper Ratio of 0.5. : Transonic-Bump Method

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Watson, James M↗

NASA NTRS1951

A Transonic-wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-fuselage Configuration Having a Wing of 60 Degree Sweepback, Aspect-ratio 4, Taper Ratio 0.6, and NACA 65A006 Airf

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Wood, Raymond B↗

NASA NTRS1950

Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected

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Stivers, Louis S , Jr↗