Aerothermodynamics of Gas Turbine and Rocket Propulsion
Aerothermodynamics of Gas Turbine and Rocket Propulsion

Author: Gordon C. Oates

Publisher: AIAA (American Institute of Aeronautics & Astronautics)

Published: 1997

Total Pages: 480

ISBN-13:

DOWNLOAD EBOOK

This seminal book on gas turbine technology has been a bestseller since it was first published. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are atmosphere programs, quasi-one-dimensional flow programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and PC given, He and PC given, isentropic expansion).

Aerothermodynamics and Jet Propulsion
Aerothermodynamics and Jet Propulsion

Author: Paul G. A. Cizmas

Publisher:

Published: 2021-11-24

Total Pages: 488

ISBN-13: 1108575595

DOWNLOAD EBOOK

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.

Gas Turbine Aero-Thermodynamics
Gas Turbine Aero-Thermodynamics

Author: F. Whittle

Publisher: Elsevier

Published: 2013-10-22

Total Pages: 276

ISBN-13: 1483293211

DOWNLOAD EBOOK

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

Fundamentals of Rocket Propulsion
Fundamentals of Rocket Propulsion

Author: DP Mishra

Publisher: CRC Press

Published: 2017-07-20

Total Pages: 462

ISBN-13: 1498785360

DOWNLOAD EBOOK

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.

Aerothermodynamics of Aircraft Engine Components
Aerothermodynamics of Aircraft Engine Components

Author: Gordon C. Oates

Publisher: AIAA

Published: 1985

Total Pages: 568

ISBN-13: 9781600860058

DOWNLOAD EBOOK

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.