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Titlebook: Gas Turbine Design, Components and System Design Integration; Meinhard T. Schobeiri Book 20181st edition Springer International Publishing

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樓主: Magnanimous
21#
發(fā)表于 2025-3-25 05:48:06 | 只看該作者
22#
發(fā)表于 2025-3-25 08:41:40 | 只看該作者
https://doi.org/10.1007/978-3-662-05822-0c flights, rocket propulsion systems and compression systems for transport of natural gas with a network of pipeline systems are a few examples of systems that heavily involve turbomachinery components.
23#
發(fā)表于 2025-3-25 13:42:47 | 只看該作者
Rechtsquellen des Arbeitsrechts, rotor blades exert forces on the working medium thereby increasing its total pressure. Based on efficiency and performance requirements, three types of compressor designs are applied. These are axial flow compressors, radial or centrifugal compressors, and mixed flow compressors.
24#
發(fā)表于 2025-3-25 18:12:23 | 只看該作者
Ihr besonderer Schutz als Mutter,onents operate near their aerodynamic, thermal, and mechanical stress limits. Under these circumstances, any adverse dynamic operation causes excessive aerodynamic, thermal, and subsequent mechanical stresses that may affect the engine safety and reliability, and, thus, the operability of the engine if adequate precautionary actions are not taken.
25#
發(fā)表于 2025-3-25 21:38:55 | 只看該作者
https://doi.org/10.1007/978-3-319-58378-5Gas Turbine; Gas Turbine Design; Turbomachinery; Turbomachinery Performance; Turbomachines
26#
發(fā)表于 2025-3-26 02:00:44 | 只看該作者
978-3-319-86392-4Springer International Publishing AG 2018
27#
發(fā)表于 2025-3-26 05:45:47 | 只看該作者
28#
發(fā)表于 2025-3-26 09:12:44 | 只看該作者
Die Voruntersuchung: Tests und Messungen,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 .. To elevate the total pressure of a working fluid, . are used that partially converts the mechanical energy into potential energy.
29#
發(fā)表于 2025-3-26 14:40:53 | 只看該作者
Albert Beyer,Christine Hofer,Ulrich TappeThe flow through a turbomachine is generally three-dimensional, viscous, highly unsteady, transitional, turbulent, and compressible. This complex flow is associated with total pressure losses caused by different flow and geometry parameters. To accurately predict the efficiency of a turbomachine, accurate flow calculation is required.
30#
發(fā)表于 2025-3-26 17:27:57 | 只看該作者
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