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標(biāo)題: Titlebook: Gas Turbine Engineering; Fundamentals, Applic Richard T. C. Harman Textbook 1981Latest edition Macmillan Publishers Limited 1981 amyotrophi [打印本頁(yè)]

作者: 吸收    時(shí)間: 2025-3-21 19:41
書(shū)目名稱(chēng)Gas Turbine Engineering影響因子(影響力)




書(shū)目名稱(chēng)Gas Turbine Engineering影響因子(影響力)學(xué)科排名




書(shū)目名稱(chēng)Gas Turbine Engineering網(wǎng)絡(luò)公開(kāi)度




書(shū)目名稱(chēng)Gas Turbine Engineering網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱(chēng)Gas Turbine Engineering被引頻次




書(shū)目名稱(chēng)Gas Turbine Engineering被引頻次學(xué)科排名




書(shū)目名稱(chēng)Gas Turbine Engineering年度引用




書(shū)目名稱(chēng)Gas Turbine Engineering年度引用學(xué)科排名




書(shū)目名稱(chēng)Gas Turbine Engineering讀者反饋




書(shū)目名稱(chēng)Gas Turbine Engineering讀者反饋學(xué)科排名





作者: 希望    時(shí)間: 2025-3-21 22:14

作者: 使激動(dòng)    時(shí)間: 2025-3-22 00:53

作者: Progesterone    時(shí)間: 2025-3-22 05:23
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.
作者: BANAL    時(shí)間: 2025-3-22 10:43
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).
作者: Barter    時(shí)間: 2025-3-22 13:38

作者: Barter    時(shí)間: 2025-3-22 20:06
,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.
作者: 成份    時(shí)間: 2025-3-23 00:42
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.
作者: Limited    時(shí)間: 2025-3-23 02:48
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.
作者: 誘惑    時(shí)間: 2025-3-23 09:17

作者: Jogging    時(shí)間: 2025-3-23 11:24

作者: upstart    時(shí)間: 2025-3-23 16:07

作者: Maximizer    時(shí)間: 2025-3-23 19:34

作者: 葡萄糖    時(shí)間: 2025-3-24 01:19
Engine Matching and Transient Characteristics,tio (and temperature ratio) could lie anywhere within the stable operating range of the compressor (section 10.1), but in practice is set at the highest practicable level to operate at high efficiency and obtain the best performance relative to weight and cost.
作者: Ambiguous    時(shí)間: 2025-3-24 04:53
The Selection of a Gas Turbine Engine,ements. Some other industries with power and heat requirements have not yet adopted gas turbine engines but could possibly benefit from their use. This chapter is written therefore for engineers without direct experience of gas turbines, and considers industrial applications only. Further informatio
作者: ESPY    時(shí)間: 2025-3-24 08:47
,Beendigung des Arbeitsverh?ltnisses,Most types of engine are designed to extract as much as possible of the energy released by the combustion of a fuel, and to deliver it in usable form at a rotating output shaft.
作者: Accomplish    時(shí)間: 2025-3-24 10:52

作者: 格言    時(shí)間: 2025-3-24 18:33
https://doi.org/10.1007/978-3-662-29360-7The axial flow compressor is the second type of dynamic compressor, whose general nature and capabilities were introduced in section 1.3. It absorbs energy from an external power source, raising the pressure of a continuous flow of working fluid by means of its blading geometry and motion.
作者: 陶瓷    時(shí)間: 2025-3-24 22:47
Schlichtungswesen und Arbeitskampf,The potentially tricky operation of dynamic compressors, with their propensity to surge, has already been mentioned in section 1.3 and chapters 5 and 6. It is a big enough subject to merit its own chapter, before the way in which the compressor is matched to the turbine and the over-all engine operating characteristics are discussed in chapter 11.
作者: 創(chuàng)新    時(shí)間: 2025-3-25 01:48

作者: 言行自由    時(shí)間: 2025-3-25 04:38

作者: Pillory    時(shí)間: 2025-3-25 10:21
Rechtsquellen des Arbeitsrechts,The thrust of a jet engine is the reaction to the rate of change of momentum imparted to the working fluid.
作者: 睨視    時(shí)間: 2025-3-25 14:59
Introduction,Most types of engine are designed to extract as much as possible of the energy released by the combustion of a fuel, and to deliver it in usable form at a rotating output shaft.
作者: Allure    時(shí)間: 2025-3-25 19:41
Applications for Gas Turbine Engines,Gas turbine engines are most generally known for their use in aircraft (section 2.1)[9] but they are also used in surface transportation (section 2.2) and increasingly in stationary applications. The latter field encompasses the greatest variety of configurations and purposes and is still expanding, whereas the aviation field is consolidating.
作者: homeostasis    時(shí)間: 2025-3-25 23:53

作者: 帳單    時(shí)間: 2025-3-26 00:24

作者: 織物    時(shí)間: 2025-3-26 08:20
Gas Turbine Engine Control,The performance parameters of a running gas turbine are determined at any time by a unique set of curves, such as those in figure 4.2. Of all the parameters shown, it is the fuel flow which is the input and which controls the operation.
作者: Limpid    時(shí)間: 2025-3-26 11:36
Gas Turbine Engine Noise Reduction,Noise is unwanted sound, generated by a vibrating surface or a turbulent flow; transmitted by synchronised pressure fluctuations through a medium (section G.1); and received by the listener’s ear or, indirectly, via a microphone and a recording and playback system.
作者: 槍支    時(shí)間: 2025-3-26 13:37

作者: 愛(ài)了嗎    時(shí)間: 2025-3-26 18:28

作者: HATCH    時(shí)間: 2025-3-26 21:45
Macmillan Publishers Limited 1981
作者: 男生戴手銬    時(shí)間: 2025-3-27 02:41

作者: 微枝末節(jié)    時(shí)間: 2025-3-27 05:34

作者: overweight    時(shí)間: 2025-3-27 11:22
Beendigung des Arbeitsverh?ltnissestroduced in sections 1.1 and 1.3: it supplies an energy input from which a part provides useful work and the remainder goes to waste as heat in the exhaust 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
作者: 要求比…更好    時(shí)間: 2025-3-27 16:18
,Besondere Arten von Arbeitsverh?ltnissen,rbine, the gas flows through an annular passage surrounding the rotating power output shaft, in a direction substantially parallel to the axis of the shaft. As the gas flows through the turbine, the blading extracts energy by the action described in section 8.2. The loss of energy causes the pressur
作者: painkillers    時(shí)間: 2025-3-27 18:12

作者: HAIL    時(shí)間: 2025-3-28 01:17
Karin Nipperdey,Reinhardt Seiferttio (and temperature ratio) could lie anywhere within the stable operating range of the compressor (section 10.1), but in practice is set at the highest practicable level to operate at high efficiency and obtain the best performance relative to weight and cost.
作者: Mindfulness    時(shí)間: 2025-3-28 06:10
,Beendigung des Arbeitsverh?ltnisses,ements. Some other industries with power and heat requirements have not yet adopted gas turbine engines but could possibly benefit from their use. This chapter is written therefore for engineers without direct experience of gas turbines, and considers industrial applications only. Further informatio
作者: 向外供接觸    時(shí)間: 2025-3-28 09:09
Das Arbeitsgericht und der Prozess, 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.
作者: sacrum    時(shí)間: 2025-3-28 13:04
https://doi.org/10.1007/978-3-663-13822-8e smallest gas turbine engines, as in some automotive or fire pump or other portable applications, and is used extensively in the smaller turbochargers. It is also suitable for turbo-expansion applications (section 2.9). Its size ranges up to about 0.15 m diameter, and its rotational speed is likely to be between 60 000 and 100 000 rev/min.
作者: 誤傳    時(shí)間: 2025-3-28 16:06
Karin Nipperdey,Reinhardt Seiferttio (and temperature ratio) could lie anywhere within the stable operating range of the compressor (section 10.1), but in practice is set at the highest practicable level to operate at high efficiency and obtain the best performance relative to weight and cost.
作者: 極為憤怒    時(shí)間: 2025-3-28 19:49

作者: FLIP    時(shí)間: 2025-3-28 23:10

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作者: Dealing    時(shí)間: 2025-3-30 02:08
,Popular Music, New Media, and the Digital Public Sphere in Kenya, C?te d’Ivoire, and Nigeria,parative perspective through our study of . music in Nigeria, . in Cote d’Ivoire, and variants of hip-hop music in Kenya, such as . and ., we seek to demonstrate how popular music articulates political processes and how musicians now exploit the opportunities new media provides. The exercise of powe
作者: orthodox    時(shí)間: 2025-3-30 05:07
Shadi M. Harb,Janise McNairspiele sowie zahlreicher Aufgaben zur selbstst?ndigen überprüfung des Wissens ist dieses Buch vor allem für Studienanf?nger sehr gut geeignet..978-3-658-37874-5978-3-658-37875-2Series ISSN 2363-9539 Series E-ISSN 2363-9547
作者: 地名表    時(shí)間: 2025-3-30 08:38

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作者: RODE    時(shí)間: 2025-3-30 17:12
Book 2015ook provides detailed descriptions of the ten known systems, illustrates them richly with examples of new spectra, and places them in the context of stellar structure and evolution..Comprised of a large cool giant plus a small hot dwarf, these key eclipsing binaries reveal fascinating changes in the




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