Liquid Rocket Engine Combustion Instability

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Liquid Rocket Engine Combustion Instability

Author : Vigor Young
Publisher : AIAA
Page : 606 pages
File Size : 45,9 Mb
Release : 1995
Category : Liquid propellant rockets
ISBN : 160086418X

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Liquid Rocket Engine Combustion Instability by Vigor Young Pdf

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

Author : Mark L. Dranovsky
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 352 pages
File Size : 52,8 Mb
Release : 2007
Category : Technology & Engineering
ISBN : 1563479214

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Combustion Instabilities in Liquid Rocket Engines by Mark L. Dranovsky Pdf

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.

Liquid Propellant Rocket Combustion Instability

Author : David T. Harrje,Frederick H. Reardon
Publisher : Unknown
Page : 674 pages
File Size : 48,9 Mb
Release : 1972
Category : Liquid propellant rockets
ISBN : UIUC:30112007520619

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Liquid Propellant Rocket Combustion Instability by David T. Harrje,Frederick H. Reardon Pdf

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.

Combustion Instability

Author : Miron Semenovich Natanzon
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 298 pages
File Size : 48,7 Mb
Release : 1999
Category : Science
ISBN : STANFORD:36105129057431

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Combustion Instability by Miron Semenovich Natanzon Pdf

First published in 1986 by Mashinostroenie, Moscow.

Internal Combustion Processes of Liquid Rocket Engines

Author : Zhen-Guo Wang
Publisher : John Wiley & Sons
Page : 392 pages
File Size : 46,5 Mb
Release : 2016-08-29
Category : Technology & Engineering
ISBN : 9781118890028

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Internal Combustion Processes of Liquid Rocket Engines by Zhen-Guo Wang Pdf

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.

Liquid Propellant Rocket Combustion Instability

Author : David T. Harrje,Frederick H. Reardon
Publisher : Unknown
Page : 637 pages
File Size : 53,5 Mb
Release : 1972
Category : Liquid propellant rockets
ISBN : LCCN:70170324

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Liquid Propellant Rocket Combustion Instability by David T. Harrje,Frederick H. Reardon Pdf

Liquid Rocket and Propellants

Author : L.E. Bollinger
Publisher : Elsevier
Page : 698 pages
File Size : 40,5 Mb
Release : 1960
Category : Science
ISBN : 9780323163330

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Liquid Rocket and Propellants by L.E. Bollinger Pdf

Liquid Rocket and Propellants

Rocket Propulsion

Author : Stephen D. Heister,William E. Anderson,Timothée L. Pourpoint,R. Joseph Cassady
Publisher : Cambridge University Press
Page : 589 pages
File Size : 55,8 Mb
Release : 2019-02-07
Category : Science
ISBN : 9781108422277

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Rocket Propulsion by Stephen D. Heister,William E. Anderson,Timothée L. Pourpoint,R. Joseph Cassady Pdf

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

Combustion Instability

Author : M. S. Natanzon
Publisher : Unknown
Page : 128 pages
File Size : 52,9 Mb
Release : 2008
Category : Aeronautics
ISBN : 1600866913

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Combustion Instability by M. S. Natanzon Pdf

Fundamental Concepts of Liquid-Propellant Rocket Engines

Author : Alessandro de Iaco Veris
Publisher : Springer Nature
Page : 747 pages
File Size : 43,7 Mb
Release : 2020-09-26
Category : Technology & Engineering
ISBN : 9783030547042

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Fundamental Concepts of Liquid-Propellant Rocket Engines by Alessandro de Iaco Veris Pdf

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.