An ejector is a technologically simple and yet wide-application fluid machine. While it has favorable characteristics for a signifficant number of technological processes, its main downside is probably its high operational energy demands. The present paper is an initial result of an ongoing research aimed at improving energy e ciency of the ejector via optimization of its geometry. In the paper, we focus mostly on presenting a general multi-objective optimization framework usable for an ejector shape optimization. The approach applicability is illustrated on a simpli ed problem comprising only a single phase flow in an ejector mixing tube and diffuser. Nevertheless, the achieved simulation and optimization results are validated against expe...
katedra: KEZ; přílohy: 1 CD; rozsah: 90 s., 9 s. přílohDiploma thesis discourse on design and optima...
<p>Optimization of small gas ejectors is typically completed by selecting a single set of operating ...
A design optimization method for turbopumps of cryogenic rocket engines has been developed. Multiobj...
This contribution deals with aerodynamic optimization using dynamic mesh method provided by Fluent s...
The shape optimisation of four CO2 ejectors is presented in this study. The considered ejectors were...
Ejectors have wide industrial application and the improvement in their efficiency is sought to incre...
The article deals with the shape optimization of a supersonic ejector for propulsion of an experimen...
International audienceCompression of a low pressure vapor without any rotating parts or direct exter...
timize ejectors is presented here. Two parameters, compression ratio and efficiency have been identi...
Advances in technological development, especially in 3D printing, allow engineers to design componen...
The performance of a diffuser in a pump stage depends on its configuration and placement within the ...
Ejector is a component using high-pressure fluid to aspirate low-pressure fluid, whose potential in ...
A study of shape optimization has become increasingly popular in academia and industry. A typical pr...
The performance of a diffuser in a pump stage depends on its configuration and placement within the ...
The aim of this paper is to develop the technical knowledge, especially the optimum geometries, for ...
katedra: KEZ; přílohy: 1 CD; rozsah: 90 s., 9 s. přílohDiploma thesis discourse on design and optima...
<p>Optimization of small gas ejectors is typically completed by selecting a single set of operating ...
A design optimization method for turbopumps of cryogenic rocket engines has been developed. Multiobj...
This contribution deals with aerodynamic optimization using dynamic mesh method provided by Fluent s...
The shape optimisation of four CO2 ejectors is presented in this study. The considered ejectors were...
Ejectors have wide industrial application and the improvement in their efficiency is sought to incre...
The article deals with the shape optimization of a supersonic ejector for propulsion of an experimen...
International audienceCompression of a low pressure vapor without any rotating parts or direct exter...
timize ejectors is presented here. Two parameters, compression ratio and efficiency have been identi...
Advances in technological development, especially in 3D printing, allow engineers to design componen...
The performance of a diffuser in a pump stage depends on its configuration and placement within the ...
Ejector is a component using high-pressure fluid to aspirate low-pressure fluid, whose potential in ...
A study of shape optimization has become increasingly popular in academia and industry. A typical pr...
The performance of a diffuser in a pump stage depends on its configuration and placement within the ...
The aim of this paper is to develop the technical knowledge, especially the optimum geometries, for ...
katedra: KEZ; přílohy: 1 CD; rozsah: 90 s., 9 s. přílohDiploma thesis discourse on design and optima...
<p>Optimization of small gas ejectors is typically completed by selecting a single set of operating ...
A design optimization method for turbopumps of cryogenic rocket engines has been developed. Multiobj...