標(biāo)題: Titlebook: Gas Turbine Design, Components and System Design Integration; Meinhard T. Schobeiri Book 20181st edition Springer International Publishing [打印本頁(yè)] 作者: Magnanimous 時(shí)間: 2025-3-21 17:58
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration影響因子(影響力)
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration影響因子(影響力)學(xué)科排名
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration網(wǎng)絡(luò)公開(kāi)度
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration網(wǎng)絡(luò)公開(kāi)度學(xué)科排名
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration被引頻次
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration被引頻次學(xué)科排名
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration年度引用
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration年度引用學(xué)科排名
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration讀者反饋
書(shū)目名稱(chēng)Gas Turbine Design, Components and System Design Integration讀者反饋學(xué)科排名
作者: 恭維 時(shí)間: 2025-3-21 22:03 作者: Guileless 時(shí)間: 2025-3-22 04:21 作者: 結(jié)合 時(shí)間: 2025-3-22 05:13 作者: AWL 時(shí)間: 2025-3-22 09:47
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.作者: CLASH 時(shí)間: 2025-3-22 12:55
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).作者: CLASH 時(shí)間: 2025-3-22 20:53
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作者: cathartic 時(shí)間: 2025-3-22 23:18 作者: 熱情的我 時(shí)間: 2025-3-23 03:12
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 ..作者: 小步舞 時(shí)間: 2025-3-23 08:46 作者: Self-Help-Group 時(shí)間: 2025-3-23 10:57
Modeling of Recuperators, Combustion Chambers, Afterburners,ocess of heat exchange occurs between the high and low temperature sides. The working principle of these components is the same ([1], [2], [3]). However, different working media are involved in the heat transfer process.作者: 重畫(huà)只能放棄 時(shí)間: 2025-3-23 16:45
Modeling the Compressor Component, Design and Off-Design,nergy, this total pressure increase requires external energy input, which must be added to the system in the form of mechanical energy. The compressor rotor blades exert forces on the working medium thereby increasing its total pressure. Based on efficiency and performance requirements, three types 作者: 鞏固 時(shí)間: 2025-3-23 20:12
Turbine Aerodynamic Design and Off-design Performance,echanical energy (shaft work) with the surroundings takes place. In contrast to compressors, the total energy of the working medium is partially converted into shaft work, thus supplying necessary power to drive the compressor component, compensate for the bearing losses and provide the net power fo作者: 沖突 時(shí)間: 2025-3-23 22:45 作者: Substance 時(shí)間: 2025-3-24 06:24
Radial Equilibrium,w as a simple radial equilibrium condition with .. .. In practice, from an aerodynamics design point of view, a constant meridional velocity component or constant total pressure may not be desirable. As an example, consider the flow field close to the hub or tip of a stage where secondary flow vortices predominate.作者: 粗鄙的人 時(shí)間: 2025-3-24 09:01
Nonlinear Dynamic Simulation of Turbomachinery Components and Systems,c flights, rocket propulsion systems and compression systems for transport of natural gas with a network of pipeline systems are a few examples of systems that heavily involve turbomachinery components.作者: 多余 時(shí)間: 2025-3-24 13:14 作者: Panacea 時(shí)間: 2025-3-24 15:27
Simulation of Gas Turbine Engines, Design Off-Design and Dynamic Performance,onents operate near their aerodynamic, thermal, and mechanical stress limits. Under these circumstances, any adverse dynamic operation causes excessive aerodynamic, thermal, and subsequent mechanical stresses that may affect the engine safety and reliability, and, thus, the operability of the engine if adequate precautionary actions are not taken.作者: lambaste 時(shí)間: 2025-3-24 19:48 作者: Insul島 時(shí)間: 2025-3-25 00:06
amic performance of gas turbines.Written by an experienced gThis 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 ava作者: guzzle 時(shí)間: 2025-3-25 05:48 作者: 可互換 時(shí)間: 2025-3-25 08:41
https://doi.org/10.1007/978-3-662-05822-0c flights, rocket propulsion systems and compression systems for transport of natural gas with a network of pipeline systems are a few examples of systems that heavily involve turbomachinery components.作者: 沒(méi)血色 時(shí)間: 2025-3-25 13:42
Rechtsquellen des Arbeitsrechts, rotor blades exert forces on the working medium thereby increasing its total pressure. Based on efficiency and performance requirements, three types of compressor designs are applied. These are axial flow compressors, radial or centrifugal compressors, and mixed flow compressors.作者: Affirm 時(shí)間: 2025-3-25 18:12
Ihr besonderer Schutz als Mutter,onents operate near their aerodynamic, thermal, and mechanical stress limits. Under these circumstances, any adverse dynamic operation causes excessive aerodynamic, thermal, and subsequent mechanical stresses that may affect the engine safety and reliability, and, thus, the operability of the engine if adequate precautionary actions are not taken.作者: conifer 時(shí)間: 2025-3-25 21:38
https://doi.org/10.1007/978-3-319-58378-5Gas Turbine; Gas Turbine Design; Turbomachinery; Turbomachinery Performance; Turbomachines作者: 賄賂 時(shí)間: 2025-3-26 02:00
978-3-319-86392-4Springer International Publishing AG 2018作者: 稱(chēng)贊 時(shí)間: 2025-3-26 05:45 作者: reaching 時(shí)間: 2025-3-26 09:12
Die Voruntersuchung: Tests und Messungen,The energy transfer in turbomachinery is established by means of the stages. A . comprises a row of fixed, guide vanes called ., and a row of rotating blades termed .. To elevate the total pressure of a working fluid, . are used that partially converts the mechanical energy into potential energy.作者: 課程 時(shí)間: 2025-3-26 14:40
Albert Beyer,Christine Hofer,Ulrich TappeThe flow through a turbomachine is generally three-dimensional, viscous, highly unsteady, transitional, turbulent, and compressible. This complex flow is associated with total pressure losses caused by different flow and geometry parameters. To accurately predict the efficiency of a turbomachine, accurate flow calculation is required.作者: MINT 時(shí)間: 2025-3-26 17:27 作者: hyperuricemia 時(shí)間: 2025-3-26 22:16 作者: Frisky 時(shí)間: 2025-3-27 02:29 作者: 災(zāi)禍 時(shí)間: 2025-3-27 06:38
Losses in Turbine and Compressor Cascades,The flow through a turbomachine is generally three-dimensional, viscous, highly unsteady, transitional, turbulent, and compressible. This complex flow is associated with total pressure losses caused by different flow and geometry parameters. To accurately predict the efficiency of a turbomachine, accurate flow calculation is required.作者: Comedienne 時(shí)間: 2025-3-27 10:56 作者: 使更活躍 時(shí)間: 2025-3-27 16:18
,Die Ermüdung als Folge der Arbeitsleistung,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.作者: 光亮 時(shí)間: 2025-3-27 19:31
Die Anpassung des Menschen an die Arbeit, gas turbine engine with its components requires solid knowledge of aero-thermodynamic, heat transfer, combustion and solid mechanics design of these components. Aerothermodynamics is the very basic tool for design, off-design and dynamic calculations of gas turbine components and hence the gas turbine system.作者: vibrant 時(shí)間: 2025-3-28 01:26 作者: Narrative 時(shí)間: 2025-3-28 06:00
Der Privatfunk im lokalen Umfeld,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.作者: 祖?zhèn)?nbsp; 時(shí)間: 2025-3-28 09:43 作者: 聽(tīng)寫(xiě) 時(shí)間: 2025-3-28 13:15 作者: 凌辱 時(shí)間: 2025-3-28 16:37 作者: exostosis 時(shí)間: 2025-3-28 22:24
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.作者: 要求比…更好 時(shí)間: 2025-3-29 01:55 作者: 售穴 時(shí)間: 2025-3-29 03:38 作者: orthodox 時(shí)間: 2025-3-29 08:15
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.作者: 打包 時(shí)間: 2025-3-29 13:50 作者: enormous 時(shí)間: 2025-3-29 18:11
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.作者: 不要不誠(chéng)實(shí) 時(shí)間: 2025-3-29 22:13
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.作者: 枯燥 時(shí)間: 2025-3-30 01:46 作者: 百科全書(shū) 時(shí)間: 2025-3-30 05:03
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).作者: left-ventricle 時(shí)間: 2025-3-30 09:05 作者: 用手捏 時(shí)間: 2025-3-30 14:57
Modeling of Inlet, Exhaust, and Pipe Systems,ategory 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.作者: 針葉樹(shù) 時(shí)間: 2025-3-30 17:22 作者: 向外供接觸 時(shí)間: 2025-3-30 20:56 作者: Intact 時(shí)間: 2025-3-31 04:20
,Die Ermüdung als Folge der Arbeitsleistung,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 conf作者: GRE 時(shí)間: 2025-3-31 09:00
Die Anpassung des Menschen an die Arbeit, gas turbine engine with its components requires solid knowledge of aero-thermodynamic, heat transfer, combustion and solid mechanics design of these components. Aerothermodynamics is the very basic tool for design, off-design and dynamic calculations of gas turbine components and hence the gas turb作者: 鞏固 時(shí)間: 2025-3-31 13:11
,Qualit?tsziele in der Augenpraxis,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.作者: 種族被根除 時(shí)間: 2025-3-31 14:03 作者: 抵消 時(shí)間: 2025-3-31 19:46
