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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
41#
發(fā)表于 2025-3-28 16:37:38 | 只看該作者
42#
發(fā)表于 2025-3-28 22:24:25 | 只看該作者
https://doi.org/10.1007/978-3-658-29939-2ategory are the connecting pipes, inlet and exhaust systems, as shown in Fig.?13.1. The function of this group consists, among other things, of the transportation of mass flow, and of converting the kinetic energy into potential energy and vice versa.
43#
發(fā)表于 2025-3-29 01:55:57 | 只看該作者
44#
發(fā)表于 2025-3-29 03:38:37 | 只看該作者
45#
發(fā)表于 2025-3-29 08:15:36 | 只看該作者
Gas Turbine Thermodynamic Process,t the connection between the turbine inlet temperature TIT, the compressor pressure ratio . and the gas turbine thermal efficiency .. Starting with a simple GT-cycles, in the following sections methods are introduced to determine the GT-efficiency and its improvement by changing the gas turbine configurations and cycles.
46#
發(fā)表于 2025-3-29 13:50:31 | 只看該作者
47#
發(fā)表于 2025-3-29 18:11:20 | 只看該作者
Turbine and Compressor Cascade Flow Forces,and compressors were treated from a unified point of view by introducing a set of dimensionless parameters. As shown in Chapter 4, the mechanical energy, and therefore the stage power, is the result of the scalar product between the moment of momentum acting on the rotor and the angular velocity.
48#
發(fā)表于 2025-3-29 22:13:09 | 只看該作者
Efficiency of Multi-Stage Turbomachines,ses determines the stage efficiency which shows the capability of energy conversion within the stage. The stage efficiency, however, is not fully identical with the efficiency of the entire turbomachine.
49#
發(fā)表于 2025-3-30 01:46:50 | 只看該作者
50#
發(fā)表于 2025-3-30 05:03:00 | 只看該作者
Blade Design,The blade geometry is adjusted to the stage velocity diagram which is designed for specific turbine or compressor flow applications. Simple blade design methods are available in the open literature (see References).
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