Автор: Gianfranco Angelino; Luigi De Luca; William A. Sir Название: Modern Research Topics in Aerospace Propulsion ISBN: 0387974172 ISBN-13(EAN): 9780387974170 Издательство: Springer Рейтинг: Цена: 26120.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Xl Publications of Corrado Casci . Thermodynamics of Refractory Material Formation by Combustion Techniques . Catalytic Combustion Processes . Combustion Modeling and Stability of Double-Base Solid Rocket Propellants . On the Anisotropy of Drop and Particle Velocity Fluctuations in Two-Phase Round Gas Jets .
Автор: He, Guo-Qiang Название: Nanomaterials in Rocket Propulsion Systems ISBN: 0128139080 ISBN-13(EAN): 9780128139080 Издательство: Elsevier Science Рейтинг: Цена: 23749.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
Nanomaterials in Rocket Propulsion Systems covers the fundamentals of nanomaterials and examines a wide range of innovative applications, presenting the current state-of-the-art in the field. Opening with a chapter on nano-sized energetic materials, the book examines metal nanoparticles-based fuels, ballistic modifiers, stabilizers and catalysts as the components of rocket propellants. Hydrogen storage materials for rocket propulsion based on nanotubes are then discussed, as are nano-porous materials and metal organic frameworks, nano-gelled propellants, nano-composite ablators and ceramic nano-composites. Other applications examined include high thermal conductivity metallic nano-composite nozzle liners, nano-emitters for Coulomb propulsion of space-crafts, and highly thermostable nano-ceramics for rocket motors.
The book finishes with coverage of combustion of nano-sized rocket fuels, nano-particles and their combustion in micro- and nano-electromechanical systems (MEMS/NEMS), plasma propulsion and nano-scale physics. Users will find this to be a valuable resource for academic and government institutions, professionals, new researchers and graduate students working in the application of nanomaterials in the aerospace industry.
Provides a detailed overview of different types of nanomaterials used in rocket propulsion, highlighting different situations in which different materials are used
Demonstrates the use of new nanomaterial concepts, allowing for an increase in payload capacity or a decrease in launch mass
Explores a range of applications using metal nanopowders, presenting a panorama on cutting-edge, technological developments
Автор: Lancaster Otis E. Название: Jet Propulsion Engines ISBN: 0691652600 ISBN-13(EAN): 9780691652603 Издательство: Wiley Рейтинг: Цена: 59400.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
Volume XII of the High Speed Aerodynamics and Jet Propulsion series. Partial Contents: Historical development of jet propulsion; basic principles of jet propulsion; analyses of the various types of jet propulsion engines including the turbojet, the turboprop, the ramjet, and intermittent jets, as well as solid and liquid propellant rocket engines and the ramrocket. Another section deals with jet driven rotors. The final sections discuss the use of atomic energy in jet propulsion and the future prospects of jet propulsion.
Originally published in 1959. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Автор: Jiun-Ming Li; Chiang Juay Teo; Boo Cheong Khoo; Ji Название: Detonation Control for Propulsion ISBN: 3319886797 ISBN-13(EAN): 9783319886794 Издательство: Springer Рейтинг: Цена: 15372.00 р. Наличие на складе: Поставка под заказ.
Описание: This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE). State-of-the-art research contributions are collected from international leading researchers devoted to the pursuit of controllable detonations for practical detonation propulsion. A system-level design of novel detonation engines, performance analysis, and advanced experimental and numerical methods are covered. In addition, the world’s first successful sled demonstration of a rocket rotating detonation engine system and innovations in the development of a kilohertz pulse detonation engine (PDE) system are reported. Readers will obtain, in a straightforward manner, an understanding of the RDE & PDE design, operation and testing approaches, and further specific integration schemes for diverse applications such as rockets for space propulsion and turbojet/ramjet engines for air-breathing propulsion. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines provides, with its comprehensive coverage from fundamental detonation science to practical research engineering techniques, a wealth of information for scientists in the field of combustion and propulsion. The volume can also serve as a reference text for faculty and graduate students and interested in shock waves, combustion and propulsion.
Автор: El-Sayed, Ahmed F. Название: Aircraft Propulsion and Gas Turbine Engines ISBN: 1466595167 ISBN-13(EAN): 9781466595163 Издательство: Taylor&Francis Рейтинг: Цена: 26796.00 р. Наличие на складе: Поставка под заказ.
Автор: Jiun-Ming Li; Chiang Juay Teo; Boo Cheong Khoo; Ji Название: Detonation Control for Propulsion ISBN: 3319689053 ISBN-13(EAN): 9783319689050 Издательство: Springer Рейтинг: Цена: 20962.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE). State-of-the-art research contributions are collected from international leading researchers devoted to the pursuit of controllable detonations for practical detonation propulsion. A system-level design of novel detonation engines, performance analysis, and advanced experimental and numerical methods are covered. In addition, the world’s first successful sled demonstration of a rocket rotating detonation engine system and innovations in the development of a kilohertz pulse detonation engine (PDE) system are reported. Readers will obtain, in a straightforward manner, an understanding of the RDE & PDE design, operation and testing approaches, and further specific integration schemes for diverse applications such as rockets for space propulsion and turbojet/ramjet engines for air-breathing propulsion. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines provides, with its comprehensive coverage from fundamental detonation science to practical research engineering techniques, a wealth of information for scientists in the field of combustion and propulsion. The volume can also serve as a reference text for faculty and graduate students and interested in shock waves, combustion and propulsion.
Автор: Edited by Kiruba Haran , Nateri Madavan , Tim C. O Название: Electrified Aircraft Propulsion ISBN: 1108419348 ISBN-13(EAN): 9781108419345 Издательство: Cambridge Academ Рейтинг: Цена: 13939.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Combining expertise from leading researchers in electric aircraft propulsion, this is an ideal introduction to cutting-edge advances and outstanding challenges in large electric aircraft design, spanning electrical engineering, materials science, design, and optimisation. A perfect resource for graduate students, researchers, and professionals.
Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects.
Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects.
Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Описание: Fully updated and revised, the second edition of this introductory text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. A state-of-the-art review of turboramjet engines, hypersonic applications, geared turbofans, and adaptive cycle engines, accompanies an examination of emissions and pollutants, greatly expanding the importance of power generation gas turbines in industrial applications, and ensuring that students will be introduced to the most current trends in the subject. With completely rewritten chapters on the operating characteristics of components and ideal and nonideal cycle analysis, additional SI units in numerous examples, new and expanded end-of-chapter problems, and updated accompanying software, this remains the ideal text for advanced undergraduate and beginning graduate students in aerospace and mechanical engineering.
Автор: Hawthorne William R., Olson Walter T. Название: Design and Performance of Gas Turbine Power Plants ISBN: 0691652473 ISBN-13(EAN): 9780691652474 Издательство: Wiley Рейтинг: Цена: 43054.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Volume XI of the High Speed Aerodynamics and Jet Propulsion series. Edited by W.R. Hawthorne and W.T. Olson. This is a comprehensive presentation of basic problems involved in the design of aircraft gas turbines, including sections covering requirements and processes, experimental techniques, fuel injection, flame stabilization, mixing processes, f
Автор: W.H.T. Loh; W.H.T. Loh Название: Jet, Rocket, Nuclear, Ion and Electric Propulsion ISBN: 3642461115 ISBN-13(EAN): 9783642461118 Издательство: Springer Рейтинг: Цена: 22359.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: During the last decade, rapid growth of knowledge in the field of jet, rocket, nuclear, ion and electric propulsion has resulted in many advances useful to the student, engineer and scientist. SUTTON who wrote Chapter 5 "Rockets and Cooling Methods," DR . Ross who wrote Chapter 8 "Advanced Nuclear Rocket Design," MR.
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