Proceedings of the National Aerospace Propulsion Conference, Sivaramakrishna
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: 46118.00 р. Наличие на складе: Нет в наличии.
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: Cizmas, Paul, Название: Aerothermodynamics & jet propulsion / ISBN: 1108480756 ISBN-13(EAN): 9781108480758 Издательство: Cambridge Academ Рейтинг: Цена: 11246.00 р. 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: 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.
Автор: Cumpsty Название: Jet Propulsion ISBN: 1107511224 ISBN-13(EAN): 9781107511224 Издательство: Cambridge Academ Рейтинг: Цена: 7918.00 р. 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.
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: Sforza, Pasquale M Название: Theory of Aerospace Propulsion ISBN: 0128093269 ISBN-13(EAN): 9780128093269 Издательство: Elsevier Science Рейтинг: Цена: 14820.00 р. 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: Calum E. Douglas, Karl Kollmann, S. Can Gulen Название: Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII ISBN: 0791884678 ISBN-13(EAN): 9780791884676 Издательство: Mare Nostrum (Eurospan) Рейтинг: Цена: 20651.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Offers a unique blend of history, technology review, theoretical fundamentals, and design guide. The subject matter is primarily piston aeroengine superchargers - developed in Germany during the Second World War (WWII) - which are centrifugal compressors driven either by the main engine crankshaft or by an exhaust gas turbine.
Автор: Tarit Bose Название: Airbreathing Propulsion ISBN: 149390180X ISBN-13(EAN): 9781493901807 Издательство: Springer Рейтинг: Цена: 9794.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This unified approach to teaching the physics of combustion, fluid dynamics and other properties of aircraft engines covers both modern and historical power units and features exercises and extensive data that allow readers to evaluate comparative results.
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.
Описание: This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs). It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.
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: 19591.00 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 .
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
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