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Results for “TAIL SURFACES”

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 91 records · Page 5

All sources NASA NTRS DOE OSTI

NASA NTRS1956

Low-speed Roll Effectiveness of a Differentially Deflected Horizontal-tail Surface on a 42 Deg Swept-wing Model

Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of differentially deflected horizontal tail

HORIZONTAL TAIL↗

NASA NTRS1951

Three papers from conference on "Wing and tail-surface oscillations : March 6-8, 1941, Munich

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CONTROLS - COMPLETE WINGS↗

NASA NTRS1961

Stability and control characteristics at transonic speeds of a model of a supersonic target drone with differentially deflected horizontal-tail surfaces

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Wornom, D. E.↗

NASA NTRS1946

Tests of a Full-scale Horizontal Tail Surface in the Langley 16-foot High-speed Tunnel

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Schueller, Carl F↗

NASA NTRS1947

Measurements of the Pressure Distribution on the Horizontal-tail Surface of a Typical Propeller-driven Pursuit Airplane in Flight I : Effects of Compressibility in Steady Straight and Accelerated Flight

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Sadoff, Melvin↗

NASA NTRS1947

Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller-driven Pursuit Airplane in Flight II : the Effect of Angle of Sideslip and Propeller Operation

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Sadoff, Melvin↗

NASA NTRS1947

Flight Tests of a Double-hinged Horizontal Tail Surface with Reference to Longitudinal-stability and Control Characteristics

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Hanson, Carl M↗

NASA NTRS1950

Experimental Investigation of the Effect of Vertical-tail Size and Length of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degree Sweptback Wing and Tail Surfaces

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Queijo, M J↗

NASA NTRS1951

Effect of horizontal-tail size and tail-length on low-speed static longitudinal stability and damping in pitch of a model having 45 degree sweptback wing and tail surfaces

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Lichtenstein, Jacob H↗

NASA NTRS1954

Calculated Subsonic Span Loads and Resulting Stability Derivatives of Unswept and 45 Degrees Sweptback Tail Surfaces in Sideslip and in Steady Roll

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Queijo, M J↗

NASA NTRS1948

Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel

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Bird, John D↗

NASA NTRS1949

Flight tests at transonic and supersonic speeds of an airplane-like configuration with thin straight sharp-edge wings and tail surfaces

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Mitchell, Jesse L↗

NASA NTRS1947

Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model

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Bird, John D↗

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 NTRS1951

Time histories of the aerodynamic loads on the vertical and horizontal tail surfaces of a jet-powered bomber airplane during sideslip maneuvers at approximately 20,000 feet

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Cooney, T V↗

NASA NTRS1951

An Investigation of the Longitudinal Characteristics of the X-3 Configuration with Wing and Horizontal Tail Surfaces of Aspect Ratio 3.0 by Means of Rocket-propelled Models : Results at High Lift Coefficients

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Peck, Robert F↗

NASA NTRS1953

A Transonic Investigation by the Free-fall Method of an Airplane Configuration Having 45 Degrees Sweptback Wing and Tail Surfaces

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Faber, Stanley↗

NASA NTRS1951

Effect of horizontal-tail location on low-speed static longitudinal stability and damping in pitch of a model having 45 degrees sweptback wing and tail surfaces

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Lichtenstein, Jacob H↗