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<metadata xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:dc="http://purl.org/dc/elements/1.1/"><dc:title>Powder particle–wall collision-based design of the discrete axial nozzle-exit shape in direct laser deposition</dc:title><dc:creator>Jeromen,	Andrej	(Avtor)
	</dc:creator><dc:creator>Vidergar,	Ana	(Avtor)
	</dc:creator><dc:creator>Fujishima,	Makoto	(Avtor)
	</dc:creator><dc:creator>Levy,	Gideon N.	(Avtor)
	</dc:creator><dc:creator>Govekar,	Edvard	(Avtor)
	</dc:creator><dc:subject>direct laser deposition</dc:subject><dc:subject>axial nozzle shapes</dc:subject><dc:subject>wall-collision-dominated flow</dc:subject><dc:subject>powder-stream distribution</dc:subject><dc:subject>powder-catchment efficiency</dc:subject><dc:description>To improve the efficiency of the direct laser deposition (DLD) of metal powders, a concentrated powder-stream distribution is required, which can be affected by the shape of the powder-delivery nozzle. In this study, a simplified, powder particle–wall collision-based 3D numerical model of the powder flow in the nozzle was used to simulate the influences of the nozzle-exit shape on the concentration of the powder stream distribution, characterized by its diameter. The nozzle-exit shape was parametrized by the exit-cone angle, length, and inner-surface roughness. Based on the simulation results, the nozzle-exit shapes of three exit-cone angles (0°, 3.5° and 7.2°), various lengths and surface-roughness values were designed. For the two larger particle sizes of 22 μm and 82 μm considered, the wall-collision-dominated regime and the influence of the nozzle-exit shape were experimentally confirmed. In particular, a significant decrease in the powder-stream diameter when increasing the divergent nozzle-exit cone angle or decreasing its surface roughness and the nonlinear influence of the cone length were shown. Using single-layer, powder-deposition experiments it was demonstrated that by modifying the design of the nozzle-exit shape, the powder-catchment efficiency was increased by 13% due to the increased nozzle-exit cone angle and by 19% due to the reduced surface roughness.</dc:description><dc:date>2022</dc:date><dc:date>2022-07-13 09:24:54</dc:date><dc:type>Članek v reviji</dc:type><dc:identifier>138253</dc:identifier><dc:identifier>UDK: 621.7</dc:identifier><dc:identifier>ISSN pri članku: 0924-0136</dc:identifier><dc:identifier>DOI: 10.1016/j.jmatprotec.2022.117704</dc:identifier><dc:identifier>COBISS_ID: 114823683</dc:identifier><dc:language>sl</dc:language></metadata>
