Creep behavior of structural joints of aircraft materials under constant loads and temperatures
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Mordfin, Leonard↗
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Results for “constant”
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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Tensile properties of Inconel X sheet under rapid-heating and constant-temperature conditions
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Kurg, Ivo M↗
Temperature and thermal-stress distributions in some structural elements heated at a constant rate
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Brooks, William A , Jr↗
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↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel II : The Effect of Constant-chord Leading- and Trailing-edge Flaps on the Low-speed Characteristics of the Wing
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Bandettini, Angelo↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel II : the Effectiveness and Hinge Moments of a Constant-chord Plain Flap
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Stephenson, Jack D↗
Investigation of performance of turbojet engine with constant- and variable-area exhaust nozzles
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Wallner, Lewis E↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel III : the Effectiveness of a Constant-chord Aileron
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Johnson, Ben H , Jr↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel IV : the Effect of a Constant-chord Leading-edge Flap at High Subsonic Speeds
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Reed, Verlin D↗
The Aerodynamic Characteristics Throughout the Subsonic Speed Range of a Thin, Sharp-edged Horizontal Tail of Aspect Ratio 4 Equipped with a Constant-chord Elevator
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Bandettini, Angelo↗
Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effects at Subsonic Speeds of a Constant-chord Elevon on a Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
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Jones, J Lloyd↗
Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds
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Sandahl, Carl A↗
The transonic characteristics of a low-aspect-ratio triangular wing with a constant-chord flap as determined by wing-flow tests, including correlation with large-scale tests
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Rathert, George A , Jr↗
Preliminary Investigation of Constant-geometry, Variable Mach Number, Supersonic Tunnel with Porous Walls
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Nelson, William J↗
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↗
Some effects of solidity on turning through constant-thickness circular-arc guide vanes in axial annular flow
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Mankuta, Harry↗
Investigation at Low Speed of the Effectiveness and Hinge Moments of a Constant-chord Elevator on a Large-scale Triangular Wing with Section Modification
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Hawes, John G↗
Preliminary Investigation of the Supersonic Flow Field Downstream of Wire-mesh Nozzles in a Constant-area Duct / Lawrence I. Gould
An investigation was conducted in a 3.4- by 3.4-inch duct to determine the characteristics of the supersonic flow downstream of four wire-mesh screen nozzles with nominal design Mach numbers in the range between 1.97 and 2.58. Two types of disturbances were observed in the flow field: a fine network of interacting expansion and compression waves which were formed immediately downstream of the screens and appeared to dissipate within 25 to 40 wave intersections; and relatively strong oblique shock waves that originated at the junctions of the screens and the walls and were reflected throughout the length of the duct. Regions of fairly uniform flow were found to exist. The total-pressure loss across the screens varied from 22 percent at Mach number 1.58 to 43 percent at Mach number 2.06.
WIND TUNNELS↗