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Author: Vigor Young Publisher: AIAA ISBN: 9781600864186 Category : Liquid propellant rockets Languages : en Pages : 606
Book Description
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: Vigor Young Publisher: AIAA ISBN: 9781600864186 Category : Liquid propellant rockets Languages : en Pages : 606
Book Description
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: Mark L. Dranovsky Publisher: AIAA (American Institute of Aeronautics & Astronautics) ISBN: 9781563479212 Category : Technology & Engineering Languages : en Pages : 352
Book Description
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 T. Harrje Publisher: ISBN: Category : Liquid propellant rockets Languages : en Pages : 674
Book Description
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 ISBN: 1118890051 Category : Technology & Engineering Languages : en Pages : 352
Book Description
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: M. R. Beltran Publisher: ISBN: Category : Hydrazines Languages : en Pages : 0
Book Description
Progress made on a study of liquid rocket engine combustion instability is presented. Particular emphasis was placed on the monomethylhydrazine-nitrogen tetroxide system. A steady-state combustion model (vaporization rate controlled) and a nonlinear combustion instability model were developed.
Author: Vigor Young
Author: Vigor Young
Author: Mark L. Dranovsky
Author: David T. Harrje
Author: 
Author: Zhen-Guo Wang
Author: David T. Harrje
Author: Luigi Crocco
Author: M. R. Beltran
Author: M. S. Natanzon
Author: Leon M. Wenzel