Автор: Cizmas, Paul, Название: Aerothermodynamics & jet propulsion / ISBN: 1108480756 ISBN-13(EAN): 9781108480758 Издательство: Cambridge Academ Рейтинг: Цена: 74970.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This robust introduction to aerothermodynamics for jet propulsion provides students with a solid theoretical foundation, consistent mathematical derivations, and example-based learning which connects key abstract concepts to practical scenarios in jet propulsion. Accompanied by online materials for course instructors.
Автор: He, Guo-Qiang Название: Nanomaterials in Rocket Propulsion Systems ISBN: 0128139080 ISBN-13(EAN): 9780128139080 Издательство: Elsevier Science Рейтинг: Цена: 158330.00 T 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: 0691626316 ISBN-13(EAN): 9780691626314 Издательство: Wiley Рейтинг: Цена: 149950.00 T 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 a
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: 102480.00 T 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: 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: 139750.00 T 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: 92930.00 T 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.
Автор: Ronald D. Flack Название: Fundamentals of Jet Propulsion with Power Generation Applications ISBN: 1316517365 ISBN-13(EAN): 9781316517369 Издательство: Cambridge Academ Рейтинг: Цена: 95030.00 T Наличие на складе: Есть у поставщика Поставка под заказ. 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.
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.
Автор: Hawthorne William R., Olson Walter T., Hawthorne W. R. Название: Design and Performance of Gas Turbine Power Plants ISBN: 0691626154 ISBN-13(EAN): 9780691626154 Издательство: Wiley Рейтинг: Цена: 100320.00 T 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: Cumpsty Название: Jet Propulsion ISBN: 1107511224 ISBN-13(EAN): 9781107511224 Издательство: Cambridge Academ Рейтинг: Цена: 52790.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book is a self-contained introduction to the design of modern civil and military jet engines through two-engine design projects for a large passenger and a new fighter aircraft. Numerous exercises, with solutions for the instructor, are included. The book emphasizes principles enriched by industrial examples from the author`s experience.
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: 149060.00 T 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.
Автор: Gomez Herrera Juan Esteban Название: Rarefied Gas Flows and Dynamic Plasma Phenomena in Electric Propulsion Systems ISBN: 3736973241 ISBN-13(EAN): 9783736973244 Издательство: Неизвестно Рейтинг: Цена: 140700.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Zu den aktuellen Entwicklungen in der Raumfahrtindustrie z hlen das stetig wachsende Interesse an miniaturisierten Satelliten sowie der immer h ufigere Einsatz elektrischer Antriebssysteme zu allgemeinen Lage- und Bahnregelungszwecken. Die Entwicklung miniaturisierter Satelliten erfordert ihrerseits den Einsatz von Antriebssystemen, die sehr kleine und pr zise zu steuernde Schubkr fte erzeugen. Vor diesem Hintergrund stellen elektrische Triebwerke eine attraktive Option dar, die Antriebsanforderungen von Satelliten sowohl in herk mmlichen als auch in miniaturisierten Gr en langfristig zu erf llen. Bei miniaturisierten Satelliten sind die Schubanforderungen oft mit niedrigen Treibstoff-Massenstromwerten und verh ltnism ig kleinen geometrischen charakteristischen L ngen verbunden. Dies kann zu verd nnten Gaszust nden innerhalb der Triebwerksd sen f hren. Wegen der hohen Komplexit t der Plasmaph nomene innerhalb elektrischer Triebwerke sowie der typischerweise hohen Rechenanforderungen, die mit der Plasmamodellierung einhergehen, werden elektrische Antriebssysteme oft auf Basis empirischer Modelle und experimenteller Daten entwickelt. Der Fokus der vorliegenden Arbeit liegt auf den oben beschriebenen Herausforderungen und den dazugeh rigen Forschungsfeldern: der Untersuchung verd nnter Gaszust nde in transsonischen Str mungen sowie der Entwicklung numerischer Modellierungsans tze zur Beschreibung des Plasmaverhaltens innerhalb elektrischer Antriebssysteme. New trends regarding fundamental design approaches of orbital spacecraft have been developing in the space industry in recent years. They include an increased interest in miniaturized satellites as well as a general rise in the use of electric propulsion systems for orbit and attitude control. The successful implementation of miniaturized satellites requires the use of propulsion devices able to provide small and precise thrust and impulse levels. One technical solution able to meet the requirements of both standa
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