Internal Combustion Processes Of Liquid Rocket Engines
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Author | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 392 |
Release | : 2016-08-29 |
Genre | : Technology & Engineering |
ISBN | : 1118890027 |
Download Internal Combustion Processes of Liquid Rocket Engines Book in PDF, Epub and Kindle
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.
Author | : Jens Metzger |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 388 |
Release | : 2017-07-31 |
Genre | : |
ISBN | : 9781977919007 |
Download Internal Combustion Processes of Liquid Rocket Engines Book in PDF, Epub and Kindle
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.
Author | : Zhen'guo Wang |
Publisher | : |
Total Pages | : 382 |
Release | : 2016 |
Genre | : Liquid propellant rocket engines |
ISBN | : 9787118110197 |
Download Internal Combustion Processes of Liquid Rocket Engines Book in PDF, Epub and Kindle
Author | : Vigor Young |
Publisher | : AIAA |
Total Pages | : 606 |
Release | : 1995 |
Genre | : Liquid propellant rockets |
ISBN | : 9781600864186 |
Download Liquid Rocket Engine Combustion Instability Book in PDF, Epub and Kindle
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.
Author | : Alessandro de Iaco Veris |
Publisher | : Springer Nature |
Total Pages | : 747 |
Release | : 2020-09-26 |
Genre | : Technology & Engineering |
ISBN | : 3030547043 |
Download Fundamental Concepts of Liquid-Propellant Rocket Engines Book in PDF, Epub and Kindle
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.
Author | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 396 |
Release | : 2016-05-17 |
Genre | : Technology & Engineering |
ISBN | : 1118890043 |
Download Internal Combustion Processes of Liquid Rocket Engines Book in PDF, Epub and Kindle
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.
Author | : David T. Harrje |
Publisher | : |
Total Pages | : 668 |
Release | : 1972 |
Genre | : Liquid propellant rockets |
ISBN | : |
Download Liquid Propellant Rocket Combustion Instability Book in PDF, Epub and Kindle
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Author | : S. LAMBIRIS |
Publisher | : |
Total Pages | : 1 |
Release | : 1962 |
Genre | : |
ISBN | : |
Download Stable Combustion Processes in Liquid Propellant Rocket Engines Book in PDF, Epub and Kindle
Information is presented on the combustion processes necessary for successful analytical modeling of liquid-propellant rocket engine combustion during stable operation. Theoretical and experimental results of single-propellant droplet combustion and their application in spray-combustion analyses are reviewed. Propellant-spray formation and droplet-size distributions from particular rocket injector types are considered. Several assumptions concerning the propellant combustion processes are examined and the experimental evidence necessary for confirming the model predictions is discussed. Recent experimental data, found sufficient for approximate model verification, are shown to be useful for guiding the development of an analytical bipropellant combustion model without the necessity of making simplifying and restrictive assumptions. A description of a new combustion model is given, which is based on detailed spatial accounting of the combustion field for each particular injector-chamber configuration and propellant combination. (Author).
Author | : Dieter K. Huzel |
Publisher | : AIAA |
Total Pages | : 452 |
Release | : 1992 |
Genre | : Liquid propellant rocket engines |
ISBN | : 9781600864001 |
Download Modern Engineering for Design of Liquid-Propellant Rocket Engines Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 0 |
Release | : 2004 |
Genre | : |
ISBN | : |
Download Combustion Processes and Instabilities in Liquid-Propellant Rocket Engines Book in PDF, Epub and Kindle
This research was directed towards developing new knowledge of combustion processes in liquid-propellant rocket engines. Attention was given to the combustion of different fuels, beginning with hydrogen-oxygen but ultimately including multicomponent hydrocarbon mixtures representative of RP fuels, and to nonlinear processes of importance in combustion instability. Effects of detailed chemical kinetics on performance and stability were addressed by introducing systematically reduced chemistry that enables theoretical analysis to be completed thoroughly and accurately. The interactions between chemistry and turbulence were addressed, including the effects of the heat release on the turbulence. The orientation of the work was fundamental and aimed at predicting not only performance and acoustic response but also intrinsic instability. The results were intended to help to improve understanding of combustion mechanisms and combustion instabilities in liquid-propellant rocket motors. The most recent specific results concern induction times in hydrogen-oxygen mixtures and heal-release effects on turbulent missing.