Internal Combustion Processes Of Liquid Rocket Engines
Download Internal Combustion Processes Of Liquid Rocket Engines full books in PDF, epub, and Kindle. Read online free Internal Combustion Processes Of Liquid Rocket Engines ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 392 |
Release | : 2016-08-29 |
Genre | : Technology & Engineering |
ISBN | : 1118890027 |
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 |
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 |
Author | : Vigor Young |
Publisher | : AIAA |
Total Pages | : 606 |
Release | : 1995 |
Genre | : Liquid propellant rockets |
ISBN | : 9781600864186 |
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 |
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 | : David T. Harrje |
Publisher | : |
Total Pages | : 668 |
Release | : 1972 |
Genre | : Liquid propellant rockets |
ISBN | : |
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 | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 396 |
Release | : 2016-05-17 |
Genre | : Technology & Engineering |
ISBN | : 1118890043 |
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 | : S. LAMBIRIS |
Publisher | : |
Total Pages | : 1 |
Release | : 1962 |
Genre | : |
ISBN | : |
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 |
Author | : David Altman |
Publisher | : Princeton University Press |
Total Pages | : 197 |
Release | : 2015-12-08 |
Genre | : Science |
ISBN | : 1400879957 |
David Altman, James M. Carter, S. S. Penner, Martin Summerfield. High Temperature Equilibrium, Expansion Processes, Combustion of Liquid Propellants, The Liquid Propellants Rocket Engine. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.