The stabilization point is located on the fuel lean side, the mixture fraction isolines are deflected around the flame base, significant entrainment of air by the fuel jet upstream of the flame stabilization point is observed and the calculated flame width becomes larger with increasing Reynolds number.
In the case of a complete disengagement, the width becomes larger (Fig. 7a).
Further increase in the ridge width results in clearly separated two rows of nanodroplets aligned along the edge of the ridges as the ridge width becomes larger than the diffusion length of Ga atoms.
For all SA values, the intensity profile was deteriorated and transversal width became larger as a function of depth with respect to the focal plane.
Our estimation of the performance of larger-scale multipliers shows that the proposed systolic multiplier achieves comparable latency to the array multiplier, using extremely smaller number of JJs when the bit-width of input becomes large.
However, this also causes a change in light intensity at the pattern edge to be attenuated, and the error of pattern line width to process change becomes large.
By comparing Fig. 1a and b with each other, we can confirm that the width of the wave function becomes large as the value of r increases.
In the high Da regime, the scaled target distribution width becomes much larger than the advection-reaction length scale and, therefore, much larger than the capture length (albeit for nonsaturated conditions, so that α Da < 1).
The results indicate that, as the ratio of the plate width to the rigid inclusion diameter becomes large about 6, the structural stress solutions along the circumference of the rigid inclusion become almost uniform.
The width of the packet for the superposition of the DSNSs becomes large as the squeezing parameter r increases.
If the proliferation area is limited to the tip of the limb bud, the limb elongates in the distal direction and the aspect ratio (length/width) becomes large.
