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Results for “Angle of attack”

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 847 records · Page 47

All sources NASA NTRS DOE OSTI

NASA NTRS1933

Wind tunnel research comparing lateral control devices, particularly at high angles of attack VIII : straight and skewed ailerons on wings with rounded tips

Tests showed the effect of the ailerons and the tip shapes on the general performance of the wing, as well as on the lateral control and stability characteristics. The hinge moments were not measured but the approximate values are given in the first report of the series.

Weick, Fred E↗

NASA NTRS1933

Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IX : tapered wings with ordinary ailerons

Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one medium and the other extreme. On each wing both medium sized tapered ailerons and short wide tapered ailerons were tested.

Weick, Fred E↗

NASA NTRS1951

Wind-Tunnel Investigation of a Number of Total Pressure Tubes at High Angles of Attack

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INSTRUMENTS - PITOT TUBES↗

NASA NTRS1951

Wind-tunnel Investigation of a Number of Total-pressure Tubes at High Angles of Attack : Subsonic Speeds

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INSTRUMENTS - PITOT TUBES - ERRORS↗

NASA NTRS1950

Supersonic flow around circular cones at angles of attack

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FLOW, SUPERSONIC↗

NASA NTRS1949

The Method of Characteristics for the Determination of Supersonic Flow over Bodies of Revolution at Small Angles of Attack

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Ferri, Antonio↗

NASA NTRS1951

Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack

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Moore, Franklin K↗

NASA NTRS1951

The Effect of Rate of Change of Angle of Attack on the Maximum Lift Coefficient of a Pursuit Airplane

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Gadeberg, Burnett L↗

NASA NTRS1952

An extension of lifting rotor theory to cover operation at large angles of attack and high inflow conditions

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Gessow, Alfred↗

NASA NTRS1952

Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips subsonic leading edges and supersonic trailing edg

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Hannah, Margery E↗

NASA NTRS1952

Span load distributions resulting from angle of attack, rolling, and pitching for tapered sweptback wings with streamwise tips

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Martin, John C↗

NASA NTRS1952

Laminar boundary layer on cone in supersonic flow at large angle of attack

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Moore, Franklin K↗

NASA NTRS1953

Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack

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WINGS, COMPLETE - ASPECT RATIO↗

NASA NTRS1953

Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack

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Stanitz, John D↗

NASA NTRS1955

Prediction of losses induced by angle of attack in cascades of sharp-nosed blades for incompressible and subsonic compressible flow

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Kramer, James J↗

NASA NTRS1954

Flight Investigation at Large Angles of Attack of the Static-pressure Errors of a Service Pitot-static Tube Having a Modified Orifice Configuration

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Gracey, William↗

NASA NTRS1954

Effects of Subsonic Mach Number on the Forces and Pressure Distributions on Four NACA 64a-series Airfoil Sections at Angles of Attack as High as 28 Degrees

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Stivers, Louis S , Jr↗

NASA NTRS1954

Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12

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Jack, John R↗