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Results for “TWIST”

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 739 records · Page 41

All sources NASA NTRS DOE OSTI

NASA NTRS1953

Pressure Distribution at Mach Numbers up to 0.90 on a Cambered and Twisted Wing Having 40 Degrees of Sweepback and an Aspect Ratio of 10, Including the Effects of Fences

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Boltz, Frederick W↗

NASA NTRS1952

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : twisted and cambered triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution

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Heitmeyer, John C↗

NASA NTRS1952

Low-speed Longitudinal Aerodynamic Characteristics of a Twisted and Cambered Wing of 45 Degree Sweepback and Aspect Ratio 8 with and Without High-lift and Stall-control Devices and a Fuselage at Reynolds Numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6

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Salmi, Reino J↗

NASA NTRS1952

The Longitudinal Characteristics at Mach Numbers up to 0.92 of a Cambered and Twisted Wing Having 40 Degrees of Sweepback and an Aspect Ratio of 10

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Edwards, George G↗

NASA NTRS1952

Effect of Camber and Twist on the Stability Characteristics of Models Having a 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds

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White, Maurice D↗

NASA NTRS1952

The Forces and Pressure Distribution at Subsonic Speeds on a Cambered and Twisted Wing Having 45 Degrees of Sweepback and Aspect Ratio of 3 and a Taper Ratio of 0.5

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Boltz, Frederick W↗

NASA NTRS1952

An Investigation of the Subsonic Speed Range of a Full-span and a Semispan Model of a Plane Wing and of a Cambered and Twisted Wing, All Having 45 Degrees of Sweepback

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Shibata, Harry H↗

NASA NTRS1953

Investigation of three tapered 45 degree sweptback cambered and twisted wings covering a simultaneous variation in aspect ratio and thickness ratio and of one related symmetrical wing at transonic speeds by the wing-flow method

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Johnson, Harold I↗

NASA NTRS1952

Effects of Twist and Camber, Fences, and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristics of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)

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Foster, Gerald V↗

NASA NTRS1952

Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45 degree sweptback wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6) as determined by pressure distributions, force tests

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Pratt, George L↗

NASA NTRS1953

Small-scale Transonic Investigation of a 45 Degree Sweptback Wing of Aspect Ratio 4 with Combinations of Nose-flap Deflections and Wing Twist

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Alford, William J , Jr↗

NASA NTRS1952

A transonic wind-tunnel investigation of the characteristics of a twisted and cambered 45 degree sweptback wing-fuselage configuration

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Harrison, Daniel E↗

NASA NTRS1953

Charts for estimation of the profile drag-lift ratio of a helicopter rotor having rectangular blades with -8 degree twist

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Gustafson, F B↗

NASA NTRS1953

The influence of a change in body shape on the effects of twist and camber as determined by a transonic wind-tunnel investigation of a 45 degree sweptback wing-fuselage configuration

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Harrison, Daniel E↗

NASA NTRS1953

Comparison of the Aerodynamic Characteristics at Transonic Speeds of a Plane Wing and a Cambered and Twisted Wing, Both Having 45 Degrees of Sweepback and an Aspect Ratio of 6

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Holdaway, George H↗

NASA NTRS1953

Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 x 10(exp 6).

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Foster, Gerald V↗

NASA NTRS1952

Summary of Some Effective Aerodynamic Twisting-moment Coefficients of Various Wing-control Configurations at Mach Numbers from 0.6 to 1.7 as Determined from Rocket-powered Models

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Strass, H Kurt↗

NASA NTRS1952

Investigation of the Low-speed Aerodynamic Characteristics of a Variable-sweep Airplane Model with a Twisted and Cambered Wing

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Becht, Robert E↗