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Titlebook: Gas Turbine Engineering; Fundamentals, Applic Richard T. C. Harman Textbook 1981Latest edition Macmillan Publishers Limited 1981 amyotrophi

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发表于 2025-3-21 19:41:50 | 显示全部楼层 |阅读模式
书目名称Gas Turbine Engineering
副标题Fundamentals, Applic
编辑Richard T. C. Harman
视频videohttp://file.papertrans.cn/381/380763/380763.mp4
图书封面Titlebook: Gas Turbine Engineering; Fundamentals, Applic Richard T. C. Harman Textbook 1981Latest edition Macmillan Publishers Limited 1981 amyotrophi
出版日期Textbook 1981Latest edition
关键词amyotrophic lateral sclerosis (ALS); engine; gas; gas turbine
版次1
doihttps://doi.org/10.1007/978-1-349-16484-4
copyrightMacmillan Publishers Limited 1981
The information of publication is updating

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The Centrifugal (Radial) Compressor,or, which compresses the fluid intermittently in separate portions, or the rotary compressor of vane or screw or other type which compresses continuously in portions separated by moving walls or boundaries.
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Combustion,haust gas. Some engines have a second combustion system which either reheats the flow for the later turbine stages (section 3.6.2), or burns more fuel in an afterburner behind the turbines to provide the high exhaust velocity required for the propulsion of supersonic aircraft (section C.6).
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,Besondere Arten von Arbeitsverhältnissen,e and temperature of the gas to fall from turbine inlet to outlet, and necessitates the use of an increasing passage area (normal to the flow) to restrain the flow to a constant velocity. This increasing area is the flare (F), shown with other typical turbine features in figure 8.1.
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The Axial Flow Turbine,e and temperature of the gas to fall from turbine inlet to outlet, and necessitates the use of an increasing passage area (normal to the flow) to restrain the flow to a constant velocity. This increasing area is the flare (F), shown with other typical turbine features in figure 8.1.
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Cycle Calculations: Design Point Performance, it may make allowance for component inefficiences, pressure losses, non-ideal behaviour of gases and numerous other effects. All these affect the performance at the design point; that is, the normal operating condition of a plant or the cruise condition of an aircraft engine.
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