In general, S-shaped prototypes and those with the H-type cross-section achieved lower angular deflection than all other prototypes, whereas those with the triangular cross-sectional shape and 32 flutes reached the greatest angular deflection.
As a result, the trapezoidal cross section has achieved an acceptable advantage and stability over the modified triangular cross section, valued as second.
The numerical result analysis indicates that using combined optimization method of lattice and exhaustion to design ash dam cross section can achieve more stable result and decrease the time consuming of calculation, which improve the performance dramatically.
For the specific hollow fiber membrane module in the present study, the inlet holes should be evenly distributed at the cross section to achieve uniform flow distribution in the module.
The result of the complete analysis shown in Figure 5(c) indicates that a 9.8 dB reduction in scattering cross section has been achieved.
After achievement of minimal value, σ sca increases and at r 1 = (2 to 3.5) r 0 cross section σ sca achieves initial value of σ sca(r 1 = r 0).
A series of velocity vector and streamline graphs of different cross-sections are achieved in the experiment.
Drastic modification of the jet cross-section was achieved by the investigated configurations, with both elliptic and triangular shapes attained downstream.
A series of velocity vectors and streamline graphs of different cross-sections are achieved for three distinct header configurations, involving conventional and improved configurations.
The measured variation in hardness, fracture toughness and cellular adhesion across the cross section confirmed the smooth transition achieved for the FGM (HAp-Al2O3-YSZ) nanocomposite, i.e. enhanced bulk toughness combined with unrestricted surface bioactivity.
Accurate total reaction cross section models are important to achieving reliable predictions from spallation and transport codes.
