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Titlebook: Axial Turbine Aerodynamics for Aero-engines; Flow Analysis and Ae Zhengping Zou,Songtao Wang,Weihao Zhang Book 2018 Springer Nature Singapo

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发表于 2025-3-23 13:19:50 | 显示全部楼层
Zhengping Zou,Songtao Wang,Weihao ZhangDescribes the comprehensive flow mechanisms in axial gas turbines in detail.Introduces both conventional and modern aerodynamic design methods.Discusses flow mechanisms and design methods of intermedi
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https://doi.org/10.1007/978-981-10-5750-2Axial Turbine; Aerothermodynamics; Aerodynamic Design; Flow Mechanisms; Boundary Layer; Secondary Flow; Sh
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978-981-13-5480-9Springer Nature Singapore Pte Ltd. and Shanghai Jiao Tong University Press 2018
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Die Malerei schwieriger Strafgefangenerigh pressure turbines, as shown in Table ., was collected from engine manuals and other materials for reference. As can be seen from the table, with the continuous development of the engines, their thrust-to-weight ratio, turbine inlet temperature, and overall pressure ratio are reaching higher and
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Die Malerei schwieriger Strafgefangener duct (ITD). The inter-turbine duct mainly serves as a flow passage, which is formed by the casing and hub, and in some occasions, the duct, together with guide vanes, also serves as a supporter and pathway of accessory pipelines. In geometry, the inter-turbine duct is an annular pipe with its two e
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https://doi.org/10.1007/978-3-211-71834-6 It also can be used as direct power output apparatus, which provides shaft power to drive a propeller, fan, or other lift or thrust equipment. In turboprop and turboshaft engine, LP turbine is also known as power turbine or free turbine. In the spatial position of the flow path, LP turbine locates
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ds.Discusses flow mechanisms and design methods of intermedi.This book is a monograph on aerodynamics of aero-engine gas turbines focusing on the new progresses on flow mechanism and design methods in the recent 20 years. Starting with basic principles in aerodynamics and thermodynamics, this book s
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Die Malerei schwieriger Strafgefangenerwith guide vanes, also serves as a supporter and pathway of accessory pipelines. In geometry, the inter-turbine duct is an annular pipe with its two ends having different diameters; the end connecting to the high-pressure turbine is its inlet, and the other end, which connects to the low-pressure turbine, is its outlet.
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