標(biāo)題: Titlebook: Jet, Rocket, Nuclear, Ion and Electric Propulsion; Theory and Design W. H. T. Loh,W. H. T. Loh Book 1968 Springer-Verlag New York Inc. 1968 [打印本頁(yè)] 作者: 烹飪 時(shí)間: 2025-3-21 16:17
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion影響因子(影響力)
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion影響因子(影響力)學(xué)科排名
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion網(wǎng)絡(luò)公開度
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion被引頻次
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion被引頻次學(xué)科排名
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion年度引用
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion年度引用學(xué)科排名
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion讀者反饋
書目名稱Jet, Rocket, Nuclear, Ion and Electric Propulsion讀者反饋學(xué)科排名
作者: 怪物 時(shí)間: 2025-3-21 22:29
g how the body coordinates the process with minimal muscular effort and deep cross-lateral connectivity. Then we are asked to reverse the pathway, starting with the foot leading behind—and again take stock of what happens and where the diagonal pathway might be broken or less fluid as we return to o作者: 逢迎春日 時(shí)間: 2025-3-22 00:39
W. H. T. Lohh (2.?=?256). As we shall see in subsequent chapters, however, one does not always carry out (that is, “run”) each possible combination; nevertheless, the principle that fewer levels per factor allows a larger number of factors to be studied still holds.作者: 束以馬具 時(shí)間: 2025-3-22 07:01
h (2.?=?256). As we shall see in subsequent chapters, however, one does not always carry out (that is, “run”) each possible combination; nevertheless, the principle that fewer levels per factor allows a larger number of factors to be studied still holds.作者: Triglyceride 時(shí)間: 2025-3-22 10:00
W. H. T. Lohh (2.?=?256). As we shall see in subsequent chapters, however, one does not always carry out (that is, “run”) each possible combination; nevertheless, the principle that fewer levels per factor allows a larger number of factors to be studied still holds.作者: 蔓藤圖飾 時(shí)間: 2025-3-22 16:31
W. H. T. Lohh (2.?=?256). As we shall see in subsequent chapters, however, one does not always carry out (that is, “run”) each possible combination; nevertheless, the principle that fewer levels per factor allows a larger number of factors to be studied still holds.作者: companion 時(shí)間: 2025-3-22 17:15 作者: CLASP 時(shí)間: 2025-3-22 22:22
ware agent simulations that are used to develop improved strategies. The chapter concludes by discussing general considerations in human and computational research, and their role in developing new human-in-the-loop design processes for complex engineering applications.作者: 內(nèi)行 時(shí)間: 2025-3-23 01:38
George P. Suttonware agent simulations that are used to develop improved strategies. The chapter concludes by discussing general considerations in human and computational research, and their role in developing new human-in-the-loop design processes for complex engineering applications.作者: THE 時(shí)間: 2025-3-23 06:36 作者: SHOCK 時(shí)間: 2025-3-23 12:51
H. S. Seifertware agent simulations that are used to develop improved strategies. The chapter concludes by discussing general considerations in human and computational research, and their role in developing new human-in-the-loop design processes for complex engineering applications.作者: SEED 時(shí)間: 2025-3-23 17:05
tribution of this chapter is an overview of the methodological challenges and core decision points when embarking on network-based design research, namely defining the overall research purpose and selecting network features. We furthermore highlight the potential for using archival data, the opportu作者: conspicuous 時(shí)間: 2025-3-23 22:02
, random transgenesis, targeted mutagenesis using embryonic stem cells and the novel genome editing techniques. It is very important for the veterinarians and technicians in charge of animal facilities, as well as for researchers and students using mouse and rat models that they have an available up作者: acrophobia 時(shí)間: 2025-3-24 01:18 作者: 沖突 時(shí)間: 2025-3-24 05:48 作者: 一罵死割除 時(shí)間: 2025-3-24 07:05 作者: HILAR 時(shí)間: 2025-3-24 14:06 作者: 健壯 時(shí)間: 2025-3-24 17:56 作者: Junction 時(shí)間: 2025-3-24 20:56
978-3-642-46111-8Springer-Verlag New York Inc. 1968作者: 復(fù)習(xí) 時(shí)間: 2025-3-25 02:40
Jet, Rocket, Nuclear, Ion and Electric Propulsion978-3-642-46109-5Series ISSN 0066-5509 作者: set598 時(shí)間: 2025-3-25 04:11 作者: 津貼 時(shí)間: 2025-3-25 10:22 作者: fatty-streak 時(shí)間: 2025-3-25 14:45 作者: Apogee 時(shí)間: 2025-3-25 15:50 作者: 階層 時(shí)間: 2025-3-25 23:35
https://doi.org/10.1007/978-3-642-46109-5aerodynamics; airplane; control; design; dynamics; electromagnetic field; energy; environment; flow; flows; je作者: 肌肉 時(shí)間: 2025-3-26 03:53
Nuclear Rocket Propulsion latter may be further subdivided into liquid-, gas-, and plasma-core engines. Although fluid-core systems have been studied by a number of investigators during the past ten years, no major development activity has been initiated. Details of these systems are discussed in Chapter 9.作者: Obstruction 時(shí)間: 2025-3-26 05:34
Radioisotope Propulsionst decades, but all except one have thus far been considered impractical. This paper briefly reviews some of these various approaches, indicates their advantages and disadvantages, and summarizes the mission capabilities and the current state of the technology of those approaches which currently appear most promising.作者: languor 時(shí)間: 2025-3-26 09:25 作者: flammable 時(shí)間: 2025-3-26 15:32 作者: 共同確定為確 時(shí)間: 2025-3-26 20:04
0066-5509 ances useful to the student, engineer and scientist. The purpose for offering this course is to make available to them these recent advances in theory and design. Accordingly, this course is organized into seven parts: Part 1 Introduction; Part 2 Jet Propulsion; Part 3 Rocket Propulsion; Part 4 Nucl作者: 諂媚于性 時(shí)間: 2025-3-26 21:35
Hybrid Rocket Theory and Design oxidizer is injected, the combustion process proceeds according to natural law and the geometric constraints designed into the grain and is not subject to external control. It is very important, therefore, to understand the details of the combustion if it is to occur in the manner desired by the designer.作者: 上坡 時(shí)間: 2025-3-27 02:50 作者: Blasphemy 時(shí)間: 2025-3-27 05:31 作者: monogamy 時(shí)間: 2025-3-27 12:25
Thermodynamic Cycle Analysis of Gas Turbines and Air-breathing Propulsion Systemsuired, the application of the unit processes to such propulsion systems will be given here, although detailed procedures within each unit process will still be omitted (here readers should refer to Chapter 1).作者: Ebct207 時(shí)間: 2025-3-27 13:44
Ramjets and Air-Augmented Rocketsface and could be used for range extension or side forces on simple bodies. For hypersonic propulsion, ramjets with internal supersonic combustion (scramjets) show great promise (see also Chapter 14).作者: Crohns-disease 時(shí)間: 2025-3-27 20:20
Rocket Classifications, Liquid Propellant Rockets, Engine Selection, and Heat Transfere, for example, a chemical combustion process of fuel with air furnishes the energy input, which is then transformed in an engine into thermal energy of a gas and subsequently by transformation into the mechanical energy through a rotating shaft and wheels to imparting momentum to the vehicle.作者: 舊石器 時(shí)間: 2025-3-28 01:47 作者: 有效 時(shí)間: 2025-3-28 05:20 作者: dysphagia 時(shí)間: 2025-3-28 08:40
Thermodynamic Cycle Analysis of Gas Turbines and Air-breathing Propulsion Systemsh intercooling, reheat, regeneration, afterburning, and water injection. These air-breathing propulsion systems can best be analyzed through thermodynamic cycle analysis. The fundamentals of thermodynamic cycle analysis were already described in detail in Chapter 1 through the various unit processes作者: Grasping 時(shí)間: 2025-3-28 12:46 作者: 古董 時(shí)間: 2025-3-28 15:09
Rocket Classifications, Liquid Propellant Rockets, Engine Selection, and Heat Transferange a constant velocity motion, or overcome retarding forces when a body is propelled through a medium. There are two essential elements in any propulsive mechanism: the energy source and an energy conversion device to transpose the energy into the form most suitable for propulsion. In an automobil作者: 無(wú)脊椎 時(shí)間: 2025-3-28 20:17
Hybrid Rocket Theory and Designlid. In a typical design (Fig. 7-1), the oxidizer is sprayed in at the head end of a solid cylindrical fuel grain. It is apparent that once the liquid oxidizer is injected, the combustion process proceeds according to natural law and the geometric constraints designed into the grain and is not subje作者: precede 時(shí)間: 2025-3-29 01:46
Nuclear Rocket Propulsion latter may be further subdivided into liquid-, gas-, and plasma-core engines. Although fluid-core systems have been studied by a number of investigators during the past ten years, no major development activity has been initiated. Details of these systems are discussed in Chapter 9.作者: sacrum 時(shí)間: 2025-3-29 03:30 作者: 敲竹杠 時(shí)間: 2025-3-29 10:51
Electric and Ion Propulsiones directly from the basic rocket equation . where ΔV = the change in velocity achieved in free space acceleration.. = exhaust velocity of the rocket... = initial mass of the rocket... = final mass of the rocket作者: TOXIC 時(shí)間: 2025-3-29 13:28
Interaction Flows Due to Supersonic Secondary Jetssor blade cascades, the analysis of the design-point operation of subsonic and supersonic inlets, etc., involve mathematically sophisticated solutions of the fluid motion and aero-thermochemical coupling between it and the medium. As difficult as some of these problems are, their basic formulation i作者: 鬧劇 時(shí)間: 2025-3-29 18:26 作者: Introduction 時(shí)間: 2025-3-29 23:25 作者: OTHER 時(shí)間: 2025-3-30 02:21 作者: Aerophagia 時(shí)間: 2025-3-30 06:31
W. H. T. Lohveral chapters, we consider designs in which all factors have two levels. Many experiments are of this type. This is because two is the minimum number of levels a factor can have and still be studied, and by having the . (2), an experiment of a certain size can include the .. After all, an experimen作者: Melanoma 時(shí)間: 2025-3-30 10:22
veral chapters, we consider designs in which all factors have two levels. Many experiments are of this type. This is because two is the minimum number of levels a factor can have and still be studied, and by having the . (2), an experiment of a certain size can include the .. After all, an experimen作者: Spangle 時(shí)間: 2025-3-30 12:57
W. H. T. Lohveral chapters, we consider designs in which all factors have two levels. Many experiments are of this type. This is because two is the minimum number of levels a factor can have and still be studied, and by having the . (2), an experiment of a certain size can include the .. After all, an experimen作者: 掙扎 時(shí)間: 2025-3-30 19:58
W. H. T. Lohveral chapters, we consider designs in which all factors have two levels. Many experiments are of this type. This is because two is the minimum number of levels a factor can have and still be studied, and by having the . (2), an experiment of a certain size can include the .. After all, an experimen
