你太谦虚 发表于 2025-3-21 19:22:22

书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine影响因子(影响力)<br>        http://figure.impactfactor.cn/if/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine影响因子(影响力)学科排名<br>        http://figure.impactfactor.cn/ifr/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine网络公开度<br>        http://figure.impactfactor.cn/at/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine网络公开度学科排名<br>        http://figure.impactfactor.cn/atr/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine被引频次<br>        http://figure.impactfactor.cn/tc/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine被引频次学科排名<br>        http://figure.impactfactor.cn/tcr/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine年度引用<br>        http://figure.impactfactor.cn/ii/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine年度引用学科排名<br>        http://figure.impactfactor.cn/iir/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine读者反馈<br>        http://figure.impactfactor.cn/5y/?ISSN=BK0867540<br><br>        <br><br>书目名称Simulation Tools and Methods for Supercritical Carbon Dioxide Radial Inflow Turbine读者反馈学科排名<br>        http://figure.impactfactor.cn/5yr/?ISSN=BK0867540<br><br>        <br><br>

AIL 发表于 2025-3-22 00:10:28

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拖网 发表于 2025-3-22 02:09:30

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ARCH 发表于 2025-3-22 05:39:10

,Development and Analysis of Design Trends for Supercritical , Radial Inflow Turbine Nozzle Guide Va 500 kW sCO. turbine rotor. Based on a number of given stator radius ratio ., blade number . and blade trailing edge thickness ., the obtained design map contains a total number of . preliminary design cases. These maps show trends of nozzle geometry and outflow that can aid a designer in selecting

thwart 发表于 2025-3-22 12:16:23

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Felicitous 发表于 2025-3-22 13:54:23

Development and Application of a Modularised Geometry Optimiser for Future Supercritical CO, Turbomrithm. The newly developed optimiser can successfully find the optimum satisfying the objective function under given weighting factors. The computational cost can be reduced through a stochastic algorithm. To validate the optimiser, a convergent-divergent nozzle for air with a target Mach number equ

烧烤 发表于 2025-3-22 20:28:45

Multi-objective Optimisation for Supercritical CO, Radial Inflow Turbine Stator,he outlet boundary patch for these stators are extracted and discussed. The Mach number distribution optimised case has the shortest divergent nozzle, and returns the best Mach number distribution and performs less loss; the outlet flow distribution optimised case has the longest divergent nozzle, a

时代错误 发表于 2025-3-22 22:40:16

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安定 发表于 2025-3-23 04:06:03

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HARP 发表于 2025-3-23 07:01:19

Jianhui Qi understanding develops by a mysterious interplay between intuitive insight and symbolic manipulation. Nonstandard analysis requires an enhanced sensitivity to the particular symbolic form that is used to ex­ press our intuitions, and so the subject poses some unique and challenging pedagogical issu
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