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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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书目名称Gas Turbine Design, Components and System Design Integration
编辑Meinhard T. Schobeiri
视频video
概述Comprehensive treatment of all aspects of gas turbine design.Presents the state-of the art component design, integration, off design and dynamic performance of gas turbines.Written by an experienced g
图书封面Titlebook: Gas Turbine Design, Components and System Design Integration;  Meinhard T. Schobeiri Book 20181st edition Springer International Publishing
描述This book written by a world-renowned expert with more than forty years of active gas turbine R&D experience comprehensively treats the design of gas turbine components and their integration into a complete system. Unlike many currently available gas turbine handbooks that provide the reader with an overview without in-depth treatment of the subject, the current book is concentrated on a detailed aero-thermodynamics, design and off-deign performance aspects of individual components as well as the system integration and its dynamic operation.This new book provides practicing gas turbine designers and young engineers working in the industry with design material that the manufacturers would keep proprietary. The book is also intended to provide instructors of turbomachinery courses around the world with a powerful tool to assign gas turbine components as project and individual modules that are integrated into a complete system. Quoting many statements by the gas turbine industryprofessionals, the young engineers graduated from the turbomachinery courses offered by the author, had the competency of engineers equivalent to three to four years of industrial experience..
出版日期Book 20181st edition
关键词Gas Turbine; Gas Turbine Design; Turbomachinery; Turbomachinery Performance; Turbomachines
版次1
doihttps://doi.org/10.1007/978-3-319-58378-5
isbn_softcover978-3-319-86392-4
isbn_ebook978-3-319-58378-5
copyrightSpringer International Publishing AG 2018
The information of publication is updating

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Incidence and Deviation,xit flow angles. We assumed that the flow is fully congruent with the blade profile. This assumption implies that the inlet and exit flow angles coincide with the camber angles at the leading and trailing edges.
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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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Radial Equilibrium,s, ф, λ, r, α. and β.. Assuming an axisymmetric flow with constant meridional velocity and total pressure distributions, we arrived at free vortex flow as a simple radial equilibrium condition with .. .. In practice, from an aerodynamics design point of view, a constant meridional velocity component
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Generic Modeling of Turbomachinery Components and Systems,t of several . that we call . ([1], [2], [3], [4]). Each component is an autonomous entity with a defined function within the system. Inlet nozzles, exit diffusers, combustion chambers, compressors, and turbines are a few component examples. A component may consist of several ..
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