Results of mechanical-properties and axial-load fatigue and fracture tests performed on thick welded plates of Inconel 718 superalloy are presented. The test objectives were to determine the tensile strength properties and the crack-growth behavior in electron-beam, plasma-arc, and gas tungsten are welds for plates 1.90 cm (0.75 in) thick. Base-metal specimens were also tested to determine the flaw-growth behavior. The tests were performed in room-temperature-air and liquid nitrogen environments. The experimental crack-growth-rate data are correlated with theoretical crack-growth-rate predictions for semielliptical surface flaws
It is well known that the introduction of sustained tensile loads during high-temperature fatigue (d...
A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...
The primary objective of this program has been to develop simple laboratory-type tests to evaluate t...
Axial load fatigue and fracture tests were conducted on thick welded plates of 2219-T87 aluminum all...
Axial load fatigue and fracture tests were conducted on thick welded plates of 2219-T87 aluminum all...
The effects of repeated weld repairs on the metallurgical characteristics, high cycle fatigue (HCF),...
Results of sustained-load environmental crack growth threshold tests performed on six spacecraft pre...
Data are presented which were developed in support of a structural assessment of NASA-LEWIS' 10-foot...
Axial load fatigue crack propagation in alloys at room, cryogenic, and high temperature
Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 17).Mode of acc...
Understanding the impact of the complex and harsh thermomechanical environment aircraft turbine engi...
[[abstract]]There are two purposes of this research: one is to compare the mechanical properties of ...
Tests to determine the tensile and fatigue properties of Inconel 718 at cryogenic temperatures show ...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The objective of the Elevated Temperature Crack Growth Program is to evaluate proposed nonlinear fra...
It is well known that the introduction of sustained tensile loads during high-temperature fatigue (d...
A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...
The primary objective of this program has been to develop simple laboratory-type tests to evaluate t...
Axial load fatigue and fracture tests were conducted on thick welded plates of 2219-T87 aluminum all...
Axial load fatigue and fracture tests were conducted on thick welded plates of 2219-T87 aluminum all...
The effects of repeated weld repairs on the metallurgical characteristics, high cycle fatigue (HCF),...
Results of sustained-load environmental crack growth threshold tests performed on six spacecraft pre...
Data are presented which were developed in support of a structural assessment of NASA-LEWIS' 10-foot...
Axial load fatigue crack propagation in alloys at room, cryogenic, and high temperature
Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 17).Mode of acc...
Understanding the impact of the complex and harsh thermomechanical environment aircraft turbine engi...
[[abstract]]There are two purposes of this research: one is to compare the mechanical properties of ...
Tests to determine the tensile and fatigue properties of Inconel 718 at cryogenic temperatures show ...
The aluminum alloy 2219-T87 has great potential for use as a cryogenic material for various manned a...
The objective of the Elevated Temperature Crack Growth Program is to evaluate proposed nonlinear fra...
It is well known that the introduction of sustained tensile loads during high-temperature fatigue (d...
A study was made to determine the effects of specimen thickness on fatigue crack growth and fracture...
The primary objective of this program has been to develop simple laboratory-type tests to evaluate t...