Preview of Behavior of Grain Boundaries in Creep of Aluminum Bicrystals


Book Description

Gliding of aluminum bicrystals along their mutual boundary was study during creep tests at 200 degrees to 650 degrees C and 1 to 100 psi. The direction of motion depends only upon the direction of maimum resloved shear stress, temperature, and degree of mismatch between orientations of the crystals. Gliding rate is cyclic and for each temperature there is a stress below which gliding does not occur. At low temperature and small orientation difference an induction period precedes gliding. Gliding operates in a relatively thick zone of crystaline metal on both sides of the boundary degenerate into bloxks that move with respect to each other, parallel to the tension axis, and that rotate about octahedral axes of the original crystal.




Grain-boundary Behavior in Creep of Aluminum Bicrystals


Book Description

The gliding of one metal crystal with respect o another parallel to their mutual grain boundary has been studied in pure aluminum bicrystals during isothermal creep at temperatures ranging from 200 to 650 degrees C under static stresses of 10 to 1,600 psi. The motion is spasmodic and begins with an induction period. Its direction is determined by that of the maximum resolved shearing stress in the plane of the grain boundary, but its rate depends as well upon the angle through which the active slip systems are bent as they cross the grain boundary. The overall gliding rate is a linear function of the cube root of time and bears and Arrhenius relationship to the temperature, and its logarithm is proportional to the stress, over small ranges of stress. Shearing occurs with a zone of finite thickness, which becomes thicker with time, increasing temperature, and increasing stress. The metal within this zone is composed of subgrains that rotate back and forth about an axis which is sometimes the octahedral axis of the parent crystal. Rupture, which is never intergranular, is preceded by a sudden increase in the rate of uniform extension in one of the crystals. The mechanism of grain-boundary gliding is described as a coordinated alternation of slip and recovery in a chain of subgrains along the grain boundary. This concept is employed to account both for the rate of primary creep and for the transition from primary to steady-state creep.










Influence of Alloying Upon Grain-boundary Creep


Book Description

Grain-boundary displacement, occurring in bicrystals during creep at elevated temperature (350 degrees c), has been measured as a function of the copper content (0.1 to 3 percent) in a series of aluminum-rich aluminum-copper solid-solution alloys. The minimums in stress and temperature, below which grain-boundary motion does not occur, increase regularly with the copper content as would be expected if recovery is necessary for movement. Otherwise, the effects, if any, of the copper solute upon grain-boundary displacement and its rate are too small for identification by the experimental technique employed. It was shown, additionally, that grain-boundary displacement appears regular and proceeds at a constant rate if observed parallel to the stress axis, whereas the motion is seen to occur in a sequence of surges and the rate to diminish with time if the observations are made perpendicular to the stress axis. This is interpreted as further evidence that grain-boundary shearing occurs within a layer of metal of finite thickness and not by sliding upon a single interface.







Technical Note


Book Description







Comparison Between Theoretical and Experimental Stresses in Circular Semimonocoque Cylinders with Rectangular Cutouts


Book Description

Comparisons are made between a theory for calculating stresses about rectangular cutouts in circular cylinders of semimonocoque construction published in NACA TN 3200 and previously published NACA experimental data. The comparisons include stresses in the stringers and shear stresses in the center of the shear panels in the neighborhood of the cutout. The theory takes into account the bending flexibility of the rings in the structure, and this factor is found to be important in the calculation of stresses about cutouts. In general, when the ring flexibility is considered, good agreement is exhibited between the calculated and experimental results.