Aerothermodynamics of Gas Turbine and Rocket Propulsion PDF Download
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Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860065
Category : Aerothermodynamics
Languages : en
Pages : 476
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Book Description
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860065
Category : Aerothermodynamics
Languages : en
Pages : 476
Get Book
Book Description
Author: Gordon C. Oates
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
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Book Description
Author: Paul G. A. Cizmas
Publisher: Cambridge University Press
ISBN: 1108480756
Category : Science
Languages : en
Pages : 487
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Book Description
This robust introduction to aerothermodynamics uses example-based teaching to provide students with a solid theoretical foundation linked to real-world engineering scenarios.
Author: F. Whittle
Publisher: Elsevier
ISBN: 1483293211
Category : Technology & Engineering
Languages : en
Pages : 276
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Book Description
For the first time simplified methods of dealing with gas turbine thermal cycles, and further theoretical innovations, have been embodied into a concise textbook. All the major aspects of the subject are covered in a comprehensive and lucid manner. Examples are included for greater clarity
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860218
Category : Aircraft gas-turbines
Languages : en
Pages : 544
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Book Description
Author: Jack D. Mattingly
Publisher: American Institute of Aeronautics and Astronautics Incorporated
ISBN: 9781624103711
Category : Aircraft gas-turbines
Languages : en
Pages : 0
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Book Description
Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Textbook coverage has been revised and expanded, including a new chapter on compressible flow. Design concepts are introduced early and integrated throughout. Written with extensive student input, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles.
Author: Gordon C. Oates
Publisher: AIAA
ISBN: 9781600860058
Category : Aerothermodynamics
Languages : en
Pages : 568
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Book Description
Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.
Author: Paul G. A. Cizmas
Publisher:
ISBN: 1108575595
Category : Science
Languages : en
Pages : 488
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Book Description
Get up to speed with this robust introduction to the aerothermodynamics principles underpinning jet propulsion, and learn how to apply these principles to jet engine components. Suitable for undergraduate students in aerospace and mechanical engineering, and for professional engineers working in jet propulsion, this textbook includes consistent emphasis on fundamental phenomena and key governing equations, providing students with a solid theoretical grounding on which to build practical understanding; clear derivations from first principles, enabling students to follow the reasoning behind key assumptions and decisions, and successfully apply these approaches to new problems; practical examples grounded in real-world jet propulsion scenarios illustrate new concepts throughout the book, giving students an early introduction to jet and rocket engine considerations; and online materials for course instructors, including solutions, figures, and software resources, to enhance student teaching.
Author: Frank Whittle
Publisher: Pergamon
ISBN: 9780080267180
Category : Aircraft gas-turbines
Languages : en
Pages : 261
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Book Description
Author: DP Mishra
Publisher: CRC Press
ISBN: 1498785360
Category : Technology & Engineering
Languages : en
Pages : 462
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Book Description
The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
