Stable Combustion Processes In Liquid Propellant Rocket Engines PDF Download
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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 | : Zhen-Guo Wang |
Publisher | : John Wiley & Sons |
Total Pages | : 509 |
Release | : 2016-05-17 |
Genre | : Technology & Engineering |
ISBN | : 1118890051 |
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 | : 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 | : David T. Harrje |
Publisher | : |
Total Pages | : 674 |
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 | : |
Publisher | : |
Total Pages | : 371 |
Release | : 1970 |
Genre | : |
ISBN | : |
Download Propellant Spray Combustion Processes During Stable and Unstable Liquid Rocket Combustion Book in PDF, ePub and Kindle
The purpose of this program is the acquisition of detailed analytical and experimental information concerning the mechanisms of energy addition from propellant spray combustion to steady flow fields and propagating pressure disturbances. Data are to be obtained and used to evaluate present or formulate new expressions describing the dynamics that contribute to the coupling processes between the spray and gas flow fields. These expressions appear in steady-state and transient propellant combustion models and bear directly on the prediction of performance and onset of high frequency combustion instability in liquid propellant rocket engines. To overcome past difficulties in comparing analytical and experimental results, an experimental apparatus which produces a monodisperse propellant spray uniformly distributed throughout the combustor has been built. The motor, to be operated as a rocket engine combustor under either stable or transient conditions, provides for optical observation and is extensively instrumented to record pressure wave amplification or decay as a function of parameter variation. Test data (drop diameters, velocity and pressure wave growth or decay as functions of chamber length and initial conditions) can be input to the newly-developed combustion models and the validity of the coupling term expressions evaluated by directly comparing the resulting predictions to experimental data. These newly-developed combustion models are described in detail.
Author | : |
Publisher | : |
Total Pages | : 668 |
Release | : 1972 |
Genre | : Space vehicles |
ISBN | : |
Download Liquid Propellant Rocket Combustion Instability Book in PDF, ePub and Kindle
Author | : Mark L. Dranovsky |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 352 |
Release | : 2007 |
Genre | : Technology & Engineering |
ISBN | : 9781563479212 |
Download Combustion Instabilities in Liquid Rocket Engines Book in PDF, ePub and Kindle
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.
Author | : David Altman |
Publisher | : Princeton University Press |
Total Pages | : 197 |
Release | : 2015-12-08 |
Genre | : Science |
ISBN | : 1400879957 |
Download Liquid Propellant Rockets Book in PDF, ePub and Kindle
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.
Author | : |
Publisher | : |
Total Pages | : 12 |
Release | : 1986 |
Genre | : |
ISBN | : |
Download プログラム射出の効果 Book in PDF, ePub and Kindle
Author | : Leon M. Wenzel |
Publisher | : |
Total Pages | : 20 |
Release | : 1965 |
Genre | : Liquid oxygen |
ISBN | : |
Download Analysis of Chugging in Liquid-bipropellant Rocket Engines Using Propellants with Different Vaporization Rates Book in PDF, ePub and Kindle