Internal Combustion Processes of Liquid Rocket Engines
Internal Combustion Processes of Liquid Rocket Engines

Author: Zhen-Guo Wang

Publisher: John Wiley & Sons

Published: 2016-08-29

Total Pages: 392

ISBN-13: 1118890027

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This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.

Fundamental Concepts of Liquid-Propellant Rocket Engines
Fundamental Concepts of Liquid-Propellant Rocket Engines

Author: Alessandro de Iaco Veris

Publisher: Springer Nature

Published: 2020-09-26

Total Pages: 747

ISBN-13: 3030547043

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This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.

Liquid Rocket Engine Combustion Instability
Liquid Rocket Engine Combustion Instability

Author: Vigor Young

Publisher: AIAA

Published: 1995

Total Pages: 606

ISBN-13: 9781600864186

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Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.

Combustion Instabilities in Liquid Rocket Engines
Combustion Instabilities in Liquid Rocket Engines

Author: Mark L. Dranovsky

Publisher: AIAA (American Institute of Aeronautics & Astronautics)

Published: 2007

Total Pages: 352

ISBN-13: 9781563479212

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This is the first book in the literature to cover the development and testing practices for liquid rocket engines in Russia and the former Soviet Union.Combustion instability represents one of the most challenging probelms in the development of propulsion engines. A famous example is the F-1 engines for the first stage of the Saturn V launch vehicles in the Apollo project. More than 2000 full engine tests and a vast number of design modifications were conducted to cure the instability problem.This book contains first-hand information about the testing and development practices for treating liquid rocket combustion-instability problems in Russia and the former Soviet Union. It covers more than 50 years of research, with an emphasis placed on the advances made since 1970.The book was prepared by a former R&D director of the Research Institute of Chemical Engineering, NIICHIMMASH, the largest liquid rocket testing center in the world, and has been carefully edited by three well-known experts in the field.

Rocket Propulsion
Rocket Propulsion

Author: Stephen D. Heister

Publisher: Cambridge University Press

Published: 2019-02-07

Total Pages: 589

ISBN-13: 1108422276

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Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.

Fundamentals of Rocket Propulsion
Fundamentals of Rocket Propulsion

Author: DP Mishra

Publisher: CRC Press

Published: 2017-07-20

Total Pages: 364

ISBN-13: 1351708414

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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.

Liquid Rocket Thrust Chambers
Liquid Rocket Thrust Chambers

Author: Vigor Yang

Publisher: AIAA (American Institute of Aeronautics & Astronautics)

Published: 2004

Total Pages: 776

ISBN-13:

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This is the first major publication on liquid-rocket combustion devices since 1960, and includes 20 chapters prepared by world-renowned experts. Each chapter focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics, and is incorporated into the volume in a well-organized, cohesive manner. There are contributions from nine different countriesChina, France, Germany, Italy, Japan, the Netherlands, Russia, Sweden, and the United States.