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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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發(fā)表于 2025-3-21 19:41:50 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書(shū)目名稱Gas Turbine Engineering
副標(biāo)題Fundamentals, Applic
編輯Richard T. C. Harman
視頻videohttp://file.papertrans.cn/381/380763/380763.mp4
圖書(shū)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
關(guān)鍵詞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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沙發(fā)
發(fā)表于 2025-3-21 22:14:18 | 只看該作者
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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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發(fā)表于 2025-3-22 10:43:02 | 只看該作者
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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發(fā)表于 2025-3-22 13:38:33 | 只看該作者
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,Besondere Arten von Arbeitsverh?ltnissen,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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發(fā)表于 2025-3-23 00:42:20 | 只看該作者
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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發(fā)表于 2025-3-23 02:48:40 | 只看該作者
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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發(fā)表于 2025-3-23 09:17:30 | 只看該作者
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