Visualization Study of Secondary Flows in Turbine Rotor Tip Regions
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Allen, Hubert W↗
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Results for “TiP”
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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Calculation of the supersonic pressure distribution on a single-curved tapered wing in regions not influenced by the root or tip
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Vincenti, Walter G↗
Some Effects of Guide-vane Turning and Stators on the Rotating Stall Characteristics of a High Hub-tip Ratio Single-stage Compressor
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Costilow, Eleanor L↗
Ground Effects on the Longitudinal Characteristics of Two Models with Wings Having Low Aspect Ratio and Pointed Tips
Wind-tunnel tests were conducted to determine the ground effects on a tailless model with a wing of aspect ratio 2 and infinite taper, and on a tailed model with a triangular wing of aspect ratio 3, with flaps. Control-surface hinge moments were measured on the tailless model. The results are compared with the predictions of the theory of Tani, et al.
CONTROLS, FLAP-TYPE - COMPLETE WINGS↗
An Experimental Investigation of the Effect of Various Parameters Including Tip Mach Number on the Flutter of Some Model Helicopter Rotor Blades
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Brooks, George W↗
Wind-tunnel Investigation of the Effect of Clipping the Tips of Triangular Wings of Different Thickness, Camber, and Aspect Ratio - Transonic Bump Method
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Emerson, Horace F↗
Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed
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Westphal, Willard R↗
Effects of compressibility on rotor hovering performance and synthesized blade-section characteristics derived from measured rotor performance of blades having NACA 0015 airfoil tip sections
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Shivers, James P↗
Performance of 24-inch supersonic axial-flow compressor in air II : performance of compressor rotor at equivalent tip speeds from 800 to 1765 feet per second
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Johnsen, Irving A↗
An Investigation at Low Speed of a 51.3 Degrees Sweptback Semispan Wing with a Raked Tip and with 16.7-percent-chord Ailerons Having Three Spans and Three Trailing-edge Angles
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Schneiter, Leslie E↗
Cooling of gas turbines I : effects of addition of fins to blade tips and rotor, admission of cooling air through part of nozzles, and change in thermal conductivity of turbine components
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Brown, W Byron↗
An Investigation of the Effect of Tip Shape on the Low-speed Aerodynamic Characteristics of Large-scale Swept Wings
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Walling, Walter C↗
Preliminary Investigation of Two Full-scale Propellers to Determine the Effect of Swept-back Blade Tips on Propeller Aerodynamic Characteristics
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Evans, Albert J↗
Performance of 24-inch Supersonic Axial-flow Compressor in Air I : Performance of Compressor Rotor at Design Tip Speed of 1600 Feet Per Second
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Ritter, William K↗
Effects of Wing-tip Turrets on the Aerodynamic Characteristics of a Typical Bomber-wing Model
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Boddy, Lee E↗
Control Effectiveness and Hinge-moment Characteristics of a Tip Control Surface on a Low-aspect-ratio Pointed Wing at a Mach Number of 1.9
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Conner, D William↗
Flight tests of a model having self-supporting fuel-carrying panels hinged to the wing tips
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Shanks, Robert E↗
Effect of Airfoil Section and Tip Tanks on the Aerodynamic Characteristics at High Subsonic Speeds of an Unswept Wing of Aspect Ratio 5.16 and Taper Ratio 0.61
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SILVERS H NORMAN↗