Results 171 to 180 of about 198,480 (259)

Experimental determination of flame length of buoyancy-controlled turbulent jet diffusion flames from inclined nozzles

Applied Thermal Engineering, 2016
Changfa Tao, Ruowen Zong
exaly   +2 more sources

Determining the uniformity and consistency of droplet size across spray drift reducing nozzles in a wind tunnel

Crop Protection, 2015
J Connor Ferguson, Chris C O'Donnell, Bhagirath Singh Chauhan   +2 more
exaly   +2 more sources

Effects of spraying pressure and installation angle of nozzles on atomization characteristics of external spraying system at a fully-mechanized mining face

Powder Technology, 2019
Aiming to effectively suppress excessively high dust concentration around the drums during coal cutting and the related dust particle dispersion issues at a fully-mechanized mining face, the present study employed experiments, numerical simulations, and ...
Shibo Yang, W. Nie, Shasha Lv, Zhiqiang Liu, Huitian Peng, Xiao Ma, P. Cai, Changwei Xu   +7 more
semanticscholar   +1 more source

CFD analysis of the hydrodynamic characteristics in a rotating packed bed with multi-nozzles

, 2020
Rotating packed bed (RPB) has been widely noted for its good mass transfer performance and tangible size savings, and its advantages are especially obvious in space-intensive scenarios, such as purification of natural gas on offshore platforms.
Wei Zhang, P. Xie, Yuxing Li, Lin Teng, Jianlu Zhu   +4 more
semanticscholar   +1 more source

The Design of the Nozzle for the Nozzle Box Microturbines

Applied Mechanics and Materials, 2015
The paper presents a comparative analysis of existing designs nozzle turbines. The advantages and disadvantages of existing designs nozzles. The description of the new nozzle design for axial microturbines. The analysis of the reasons for reducing the loss of kinetic energy of the flow of the working fluid in the nozzles of the proposed design offers.
Andrey Yu. Fershalov, Mikhail Yu. Fershalov, Yuriy Ya. Fershalov, Timofey V. Sazonov, Damir I. Ibragimov   +4 more
openaire   +1 more source

Mathematical model for multivariate nonlinear prediction of SMD of X-type swirl pressure nozzles

Chemical engineering research & design, 2019
X-type swirl pressure nozzle is a new type of nozzle with the spin core structure. Due to its superior atomization characteristics, it has been widely applied in the field of spraying dust suppression in recent years.
Pengfei Wang, Chang Tian, Rong-hua Liu, Jian Wang   +3 more
semanticscholar   +1 more source

Study on the performance of a rotating detonation chamber with different aerospike nozzles

, 2020
To generate thrust efficiently is the ultimate objective of developing a practical propulsion device utilizing detonation. The rotating detonation engine shows its great potentials because of pressure gain combustion is produced while detonations rotate ...
Yiyuan Zhu, Ke Wang, Wang Zhicheng, Minghao Zhao, Zhongtian Jiao, Yun Wang, W. Fan   +6 more
semanticscholar   +1 more source

Steam Flow in Nozzle and the Nozzle Calculation

Applied Mechanics and Materials, 2013
The adiabatic flow process of gas or steam in a nozzle is not only widely used in steam turbines or other power equipment, but also applied to ejectors, impeller-type compressors, burners and other thermal devices in air conditioning, ventilation and gas engineering.
Ya Rong Wang, Pei Rong Wang
openaire   +1 more source

Fine spherical powder production during gas atomization of pressurized melts through melt nozzles with a small inner diameter

Powder Technology, 2019
A pressure-gas atomizer was developed, in which the melts were pressurized through melt nozzles with a small inner diameter, aiming for a small mass median diameter (MMD, d50,3) and high productivity of fine spherical powders.
Xing-gang Li, Qiang Zhu, Shih-Hung Shu, Jianzhong Fan, Shao-ming Zhang   +4 more
semanticscholar   +1 more source

Performance of a Rotating Detonation Rocket Engine with Various Convergent Nozzles and Chamber Lengths

Energies, 2019
A rotating detonation rocket engine (RDRE) with various convergent nozzles and chamber lengths is investigated. Three hundred hot-fire tests are performed using methane and oxygen ranging from equivalence ratio equaling 0.5–2.5 and total propellant flow ...
J. Bennewitz, Blaine Bigler, M. Ross, S. Danczyk, W. Hargus, Richard D. Smith   +5 more
semanticscholar   +1 more source