Aerospace Propulsion

Aerospace Propulsion PDF
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Author: T. W. Lee
Publisher: John Wiley & Sons
ISBN: 1118307984
Size: 34.66 MB
Format: PDF, Mobi
Category : Technology & Engineering
Languages : en
Pages : 316
View: 5342



Aerospace Propulsion Systems

Aerospace Propulsion Systems PDF
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Author: Thomas A. Ward
Publisher: John Wiley & Sons
ISBN: 0470824972
Size: 24.86 MB
Format: PDF, ePub, Docs
Category : Technology & Engineering
Languages : en
Pages : 448
View: 1011

Aerospace Propulsion Systems is a unique book focusing on each type of propulsion system commonly used in aerospace vehicles today: rockets, piston aero engines, gas turbine engines, ramjets, and scramjets. Dr. Thomas A. Ward introduces each system in detail, imparting an understanding of basic engineering principles, describing key functionality mechanisms used in past and modern designs, and provides guidelines for student design projects. With a balance of theory, fundamental performance analysis, and design, the book is specifically targeted to students or professionals who are new to the field and is arranged in an intuitive, systematic format to enhance learning. Covers all engine types, including piston aero engines Design principles presented in historical order for progressive understanding Focuses on major elements to avoid overwhelming or confusing readers Presents example systems from the US, the UK, Germany, Russia, Europe, China, Japan, and India Richly illustrated with detailed photographs Cartoon panels present the subject in an interesting, easy-to-understand way Contains carefully constructed problems (with a solution manual available to the educator) Lecture slides and additional problem sets for instructor use Advanced undergraduate students, graduate students and engineering professionals new to the area of propulsion will find Aerospace Propulsion Systems a highly accessible guide to grasping the key essentials. Field experts will also find that the book is a very useful resource for explaining propulsion issues or technology to engineers, technicians, businessmen, or policy makers. Post-graduates involved in multi-disciplinary research or anybody interested in learning more about spacecraft, aircraft, or engineering would find this book to be a helpful reference. Lecture materials for instructors available at www.wiley.com/go/wardaero


Theory Of Aerospace Propulsion

Theory of Aerospace Propulsion PDF
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Author: Pasquale M Sforza
Publisher: Butterworth-Heinemann
ISBN: 0128096012
Size: 37.38 MB
Format: PDF
Category : Technology & Engineering
Languages : en
Pages : 848
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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. Includes broader coverage than that found in most other books, including coverage of propellers, nuclear rockets, and space propulsion to allows analysis and design of more types of propulsion systems Provides in-depth, quantitative treatments of the components of jet propulsion engines, including the tools for evaluation and component matching for optimal system performance Contains additional worked examples and progressively challenging end-of- chapter exercises that provide practice for analysis, preliminary design, and systems integration


Powered Flight

Powered Flight PDF
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Author: David R. Greatrix
Publisher: Springer Science & Business Media
ISBN: 1447124847
Size: 12.32 MB
Format: PDF
Category : Technology & Engineering
Languages : en
Pages : 526
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Whilst most contemporary books in the aerospace propulsion field are dedicated primarily to gas turbine engines, there is often little or no coverage of other propulsion systems and devices such as propeller and helicopter rotors or detailed attention to rocket engines. By taking a wider viewpoint, Powered Flight - The Engineering of Aerospace Propulsion aims to provide a broader context, allowing observations and comparisons to be made across systems that are overlooked by focusing on a single aspect alone. The physics and history of aerospace propulsion are built on step-by-step, coupled with the development of an appreciation for the mathematics involved in the science and engineering of propulsion. Combining the author’s experience as a researcher, an industry professional and a lecturer in graduate and undergraduate aerospace engineering, Powered Flight - The Engineering of Aerospace Propulsion covers its subject matter both theoretically and with an awareness of the practicalities of the industry. To ensure that the content is clear, representative but also interesting the text is complimented by a range of relevant graphs and photographs including representative engineering, in addition to several propeller performance charts. These items provide excellent reference and support materials for graduate and undergraduate projects and exercises. Students in the field of aerospace engineering will find that Powered Flight - The Engineering of Aerospace Propulsion supports their studies from the introductory stage and throughout more intensive follow-on studies.


Theory Of Aerospace Propulsion

Theory of Aerospace Propulsion PDF
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Author: P. M. Sforza
Publisher: Elsevier
ISBN: 1856179125
Size: 39.34 MB
Format: PDF, ePub
Category : Technology & Engineering
Languages : en
Pages : 684
View: 6732

Readers of this book will be able to: utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems and be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions, perform preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. Early coverage of cycle analysis provides a systems perspective, and offers context for the chapters on turbomachinery and components Broader coverage than found in most other books - including coverage of propellers, nuclear rockets, and space propulsion - allows analysis and design of more types of propulsion systems In depth, quantitative treatments of the components of jet propulsion engines provides the tools for evaluation and component matching for optimal system performance Worked examples and end of chapter exercises provide practice for analysis, preliminary design, and systems integration


Air Breathing Engines And Aerospace Propulsion

Air Breathing Engines and Aerospace Propulsion PDF
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Author: B. N. Raghunandan
Publisher: Allied Publishers
ISBN: 9788177646900
Size: 77.10 MB
Format: PDF, Mobi
Category : Aircraft gas-turbines
Languages : en
Pages : 717
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Contributed papers presented at the 7th National Conference on Air Breathing Engines and Aerospace Propulsion, hosted at I.I.T., Kanpur.


Modern Research Topics In Aerospace Propulsion

Modern Research Topics in Aerospace Propulsion PDF
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Author: Gianfranco Angelino
Publisher: Springer Science & Business Media
ISBN: 1461209455
Size: 66.40 MB
Format: PDF
Category : Technology & Engineering
Languages : en
Pages : 375
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This volume, published in honor of Professor Corrado Casci, celebrates the life of a very distinguished international figure devoted to sCientific study, research, teaching, and leadership. The numerous contributions of Corrado CasCi are widely admired by scientists and engineers around the globe. He has been an impressive model and outstanding colleague to many researchers. Unfortunately, only a few of them could be invited to contribute to this honorific volume. Everyone of the invited contributors responded with enthusiasm. v Corrado Casci Contents Preface. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v Contributors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IX Curriculum Vitae . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Xl Publications of Corrado Casci . . . . . . . . . . . . . . . . . . . . . . . . . . . xix . . . . . . . . . I. Combustion 1. Mechanics of Turbulent Flow in Combustors for Premixed Gases . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 A. K. OPPENHEIM 2. A Pore-Structure-Independent Combustion Model for Porous Media with Application to Graphite Oxidation 19 M. B. RICHARDS AND S. S. PENNER 3. Stabilization of Hydrogen-Air Flames in Supersonic Flow. . 37 G. WINTERFELD 4. Thermodynamics of Refractory Material Formation by Combustion Techniques . . . . . . . . . . . . . . . . . . . . . . . . . . 49 I. GLASSMAN, K. BREZINSKY, AND K. A. DAVIS 5. Catalytic Combustion Processes . . . . . . . . . . . . . . . . . . . . . . 63 A. P. GLASKOVA 6. Stability of Ignition Transients of Reactive Solid Mixtures 83 V. E. ZARKO 7. Combustion Modeling and Stability of Double-Base Solid Rocket Propellants . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 109 L. DE LUCA AND L. GALFETTI 8. Combustion Instabilities and Rayleigh's Criterion 135 F. E. C. CULICK II. Liquid Sprays 9. On the Anisotropy of Drop and Particle Velocity Fluctuations in Two-Phase Round Gas Jets . . . . . . . . . . . . . 155 A. TOMBOULIDES, M. l ANDREWS, AND F. V. BRACCO vii viii Contents 10.


Aerospace Propulsion

Aerospace Propulsion PDF
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Author: T. W. Lee
Publisher: John Wiley & Sons
ISBN: 1118534875
Size: 34.59 MB
Format: PDF, Mobi
Category : Technology & Engineering
Languages : en
Pages : 320
View: 1586

Aerospace propulsion devices embody some of the most advancedtechnologies, ranging from materials, fluid control, and heattransfer and combustion. In order to maximize the performance,sophisticated testing and computer simulation tools are developedand used. Aerospace Propulsion comprehensively covers the mechanicsand thermal-fluid aspects of aerospace propulsion, starting fromthe fundamental principles, and covering applications togas-turbine and space propulsion (rocket) systems. It presentsmodern analytical methods using MATLAB and other advanced softwareand includes essential elements of both gas-turbine and rocketpropulsion systems. Gas turbine coverage includes thermodynamicanalysis, turbine components, diffusers, compressors, turbines,nozzles, compressor-turbine matching, combustors and afterburners.Rocket coverage includes chemical rockets, electrical rockets,nuclear and solar sail. Key features: Both gas-turbine and rocket propulsion covered in a singlevolume Presents modern analytical methods and examples Combines fundamentals and applications, including spaceapplications Accompanied by a website containing MATLAB examples, problemsets and solutions Aerospace Propulsion is a comprehensive textbook forsenior undergraduate graduate and aerospace propulsion courses, andis also an excellent reference for researchers and practicingengineers working in this area.


Materials Needs And R D Strategy For Future Military Aerospace Propulsion Systems

Materials Needs and R D Strategy for Future Military Aerospace Propulsion Systems PDF
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Author: National Research Council
Publisher: National Academies Press
ISBN: 0309212111
Size: 61.44 MB
Format: PDF, Docs
Category : Technology & Engineering
Languages : en
Pages : 214
View: 4915

The ongoing development of military aerospace platforms requires continuous technology advances in order to provide the nation's war fighters with the desired advantage. Significant advances in the performance and efficiency of jet and rocket propulsion systems are strongly dependent on the development of lighter more durable high-temperature materials. Materials development has been significantly reduced in the United States since the early 1990s, when the Department of Defense (DOD), the military services, and industry had very active materials development activities to underpin the development of new propulsion systems. This resulted in significant improvements in all engine characteristics and established the United States in global propulsion technology. Many of the significant advances in aircraft and rocket propulsion have been enabled by improved materials and, materials manufacturing processes. To improve efficiency further, engine weight must be reduced while preserving thrust. Materials Needs and Research and Development Strategy for Future Military Aerospace Propulsion Systems examines whether current and planned U.S. efforts are sufficient to meet U.S. military needs while keeping the U.S. on the leading edge of propulsion technology. This report considers mechanisms for the timely insertion of materials in propulsion systems and how these mechanisms might be improved, and describes the general elements of research and development strategies to develop materials for future military aerospace propulsion systems. The conclusions and recommendations asserted in this report will enhance the efficiency, level of effort, and impact of DOD materials development activities.


Proceedings Of The National Aerospace Propulsion Conference

Proceedings of the National Aerospace Propulsion Conference PDF
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Author: Chetan S. Mistry
Publisher: Springer Nature
ISBN: 9811550395
Size: 50.21 MB
Format: PDF
Category : Technology & Engineering
Languages : en
Pages : 546
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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. The papers cover aerospace propulsion-related topics, and discuss relevant research advances made in this field. It will be of interest to researchers in industry and academia working on gas turbine, rocket, and jet engines.