Design and Development of Aerospace Vehicles and Propulsion Systems: Proceedings of SAROD 2018, Kumar S. Kishore, Narayanaswamy Indira, Ramesh V.
Автор: Pini Matteo, de Servi Carlo, Spinelli Andrea Название: Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power: Nicfd 2020 ISBN: 3030693058 ISBN-13(EAN): 9783030693053 Издательство: Springer Цена: 139750.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book contains a collection of the main contributions from the third edition of the NICFD conference, organized by the Special Interest Group on Non-Ideal Compressible Fluid Dynamics (SIG-49).
Автор: Lee Название: Aerospace Propulsion ISBN: 1118307984 ISBN-13(EAN): 9781118307984 Издательство: Wiley Рейтинг: Цена: 75980.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Aerospace propulsion devices embody some of the most advanced technologies, ranging from materials, fluid control, and heat transfer and combustion. In order to maximize the performance, sophisticated testing and computer simulation tools are developed and used.
Автор: Kumar S. Kishore, Narayanaswamy Indira, Ramesh V. Название: Design and Development of Aerospace Vehicles and Propulsion Systems: Proceedings of Sarod 2018 ISBN: 981159600X ISBN-13(EAN): 9789811596001 Издательство: Springer Цена: 316790.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due To Chevron.- Parametric Study of Turbulent Flow Past a Compression Decompression Ramp.- Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake.- Aero-Elastic Analysis of High Aspect Ratio UAV Wing - Based on Two-Way Fluid Structure Interaction.- Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade.- Effect of Incoming Wakes on Losses of a Low Pressure Turbine of a Gas Turbine Engine.- Effect of Axial Location on the Performance of A Control Jet In A Supersonic Cross Flow
Автор: Mistry Chetan S., Kumar S. Kishore, Raghunandan B. N. Название: Proceedings of the National Aerospace Propulsion Conference ISBN: 9811550387 ISBN-13(EAN): 9789811550386 Издательство: Springer Цена: 307450.00 T Наличие на складе: Поставка под заказ. Описание: This volume presents selected papers presented during the National Aerospace Propulsion Conference (NAPC) held at Indian Institute of Technology Kharagpur. It brings together contributions from the entire propulsion community, spanning air-breathing and non-air-breathing propulsion.
Автор: Hunley Название: The Development Of Propulsion Technology For U.S. Space-Launch Vehicles, 1 ISBN: 1603449876 ISBN-13(EAN): 9781603449878 Издательство: Mare Nostrum (Eurospan) Рейтинг: Цена: 38810.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: In this definitive study, J. D. Hunley traces the program's development from Goddard's early rockets (and the German V-2 missile) through the Titan IVA and the Space Shuttle, with a focus on space-launch vehicles. Since these rockets often evolved from early missiles, he pays considerable attention to missile technology, not as an end in itself, but as a contributor to launch-vehicle technology. Focusing especially on the engineering culture of the program, Hunley communicates this very human side of technological development by means of anecdotes, character sketches, and case studies of problems faced by rocket engineers. He shows how such a highly adaptive approach enabled the evolution of a hugely complicated technology that was impressive-but decidedly not rocket science. Unique in its single-volume coverage of the evolution of launch-vehicle technology from 1926 to 1991, this meticulously researched work will inform scholars and engineers interested in the history of technology and innovation, as well as those specializing in the history of space flight. J. D. HUNLEY's career as a historian has focused on the history of aerospace technology. He was named a Ramsey Fellow at the National Air and Space Museum for 2001-2002 after serving in history programs for both NASA and the U.S. Air Force. He holds a Ph.D. from the University of Virginia. Now semiretired, he continues to write about the history of America's space program
Автор: Ward Название: Aerospace Propulsion Systems ISBN: 0470824972 ISBN-13(EAN): 9780470824979 Издательство: Wiley Рейтинг: Цена: 116110.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Aerospace Propulsion Systems is a unique book that focuses on propulsion systems commonly used in aerospace vehicles today; e.g. , rockets, piston aero engines, gas turbine engines, ramjets, and scramjets.
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: 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: Pini Matteo, de Servi Carlo, Spinelli Andrea Название: Proceedings of the 3rd International Seminar on Non-Ideal Compressible Fluid Dynamics for Propulsion and Power: Nicfd 2020 ISBN: 3030693082 ISBN-13(EAN): 9783030693084 Издательство: Springer Рейтинг: Цена: 139750.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book contains a collection of the main contributions from the third edition of the NICFD conference, organized by the Special Interest Group on Non-Ideal Compressible Fluid Dynamics (SIG-49).
Автор: Sforza, Pasquale M Название: Theory of Aerospace Propulsion ISBN: 0128093269 ISBN-13(EAN): 9780128093269 Издательство: Elsevier Science Рейтинг: Цена: 98800.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание:
Theory of Aerospace Propulsion, Second Edition, teaches engineering students how to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems, be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions and preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. This updated edition has been fully revised, with new content, new examples and problems, and improved illustrations to better facilitate learning of key concepts.
Автор: Gianfranco Angelino; Luigi De Luca; William A. Sir Название: Modern Research Topics in Aerospace Propulsion ISBN: 1461269563 ISBN-13(EAN): 9781461269564 Издательство: Springer Рейтинг: Цена: 130610.00 T 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: 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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