Corrugate
发表于 2025-3-21 16:39:26
书目名称Gas Turbine Design, Components and System Design Integration影响因子(影响力)<br> http://impactfactor.cn/2024/if/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration影响因子(影响力)学科排名<br> http://impactfactor.cn/2024/ifr/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration网络公开度<br> http://impactfactor.cn/2024/at/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration网络公开度学科排名<br> http://impactfactor.cn/2024/atr/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration被引频次<br> http://impactfactor.cn/2024/tc/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration被引频次学科排名<br> http://impactfactor.cn/2024/tcr/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration年度引用<br> http://impactfactor.cn/2024/ii/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration年度引用学科排名<br> http://impactfactor.cn/2024/iir/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration读者反馈<br> http://impactfactor.cn/2024/5y/?ISSN=BK0380761<br><br> <br><br>书目名称Gas Turbine Design, Components and System Design Integration读者反馈学科排名<br> http://impactfactor.cn/2024/5yr/?ISSN=BK0380761<br><br> <br><br>
陪审团
发表于 2025-3-21 23:58:54
Die Berufskrankheiten in der Schweiz,The energy transfer in turbomachinery is established by means of the stages. A . comprises a row of fixed, guide vanes called ., and a row of rotating blades termed ..
Morphine
发表于 2025-3-22 02:44:07
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外表读作
发表于 2025-3-22 08:07:40
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In-Situ
发表于 2025-3-22 09:51:17
Arbeitsmethoden der ThermodynamikUp to this point, the relationships developed for a turbomachinery stage have been strictly correct for given velocity diagrams with known inlet and exit flow angles. We assumed that the flow is fully congruent with the blade profile.
MERIT
发表于 2025-3-22 14:04:15
https://doi.org/10.1007/978-3-322-89473-1This chapter deals with the numerical modeling of the components pertaining to group 1 discussed in section 13.1.1. The components pertaining to this category are the connecting pipes, inlet and exhaust systems, as shown in Figure 13.1
MERIT
发表于 2025-3-22 19:41:48
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Tracheotomy
发表于 2025-3-22 23:32:17
Gas Turbine Thermodynamic Process,The first step toward designing a new gas turbine is to generate its thermodynamic cycle diagram. This diagram provides the essential information about the connection between the turbine inlet temperature TIT, the compressor pressure ratio . and the gas turbine thermal efficiency ..
贝雷帽
发表于 2025-3-23 05:19:21
Theory of Turbomachinery Stages,The energy transfer in turbomachinery is established by means of the stages. A . comprises a row of fixed, guide vanes called ., and a row of rotating blades termed ..
Munificent
发表于 2025-3-23 06:57:14
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