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Liquid Rocket Engine Combustion Instability


Liquid Rocket Engine Combustion Instability
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Combustion Instabilities In Liquid Rocket Engines


Combustion Instabilities In Liquid Rocket Engines
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Author : Mark L. Dranovsky
language : en
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Release Date : 2007

Combustion Instabilities In Liquid Rocket Engines written by Mark L. Dranovsky and has been published by AIAA (American Institute of Aeronautics & Astronautics) this book supported file pdf, txt, epub, kindle and other format this book has been release on 2007 with Technology & Engineering categories.


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 Rocket Engine Combustion Instability


Liquid Rocket Engine Combustion Instability
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Author : Vigor Young
language : en
Publisher: AIAA
Release Date : 1995

Liquid Rocket Engine Combustion Instability written by Vigor Young and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Liquid propellant rockets categories.


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 Instability


Combustion Instability
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Author : Miron Semenovich Natanzon
language : en
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Release Date : 1999

Combustion Instability written by Miron Semenovich Natanzon and has been published by AIAA (American Institute of Aeronautics & Astronautics) this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Science categories.


First published in 1986 by Mashinostroenie, Moscow.



Liquid Propellant Rocket Combustion Instability


Liquid Propellant Rocket Combustion Instability
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Author : David T. Harrje
language : en
Publisher:
Release Date : 1972

Liquid Propellant Rocket Combustion Instability written by David T. Harrje and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Liquid propellant rockets categories.


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.



Rocket Propulsion


Rocket Propulsion
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Author : Stephen D. Heister
language : en
Publisher: Cambridge University Press
Release Date : 2019-02-07

Rocket Propulsion written by Stephen D. Heister and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2019-02-07 with Science categories.


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



Modern Engineering For Design Of Liquid Propellant Rocket Engines


Modern Engineering For Design Of Liquid Propellant Rocket Engines
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Author : Dieter K. Huzel
language : en
Publisher: AIAA
Release Date : 1992

Modern Engineering For Design Of Liquid Propellant Rocket Engines written by Dieter K. Huzel and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Liquid propellant rocket engines categories.




Analysis Of Liquid Rocket Engine Combustion Instability


Analysis Of Liquid Rocket Engine Combustion Instability
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Author : M. R. Beltran
language : en
Publisher:
Release Date : 1966

Analysis Of Liquid Rocket Engine Combustion Instability written by M. R. Beltran and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.


This report develops a nonlinear model which can be used to predict combustion instability zones in liquid rocket engines. The model is developed by combining a nonlinear instability model with a steady-state vaporization model. Such an analysis determines the zones of an engine in which a tangential mode of high frequency instability is most easily initiated. A rocket engine can be analyzed by incrementally dividing the combustion chamber into annular nodes in the r and z directions. Steady-state properties at each annular node or position in the chamber are computed from the steady-state vaporization computer program. The steady-state program is capable of computing combustion profiles in thermally unstable propellants of the monomethylhydrazine/nitrogen tetroxide type. This model describes droplet vaporization with vapor phase decomposition. Using the computed steady-state properties and the stability limit curves from the instability computer program, stability at each node is determined. This process is repeated for each node to determine a stability map of the entire engine.



Progress In Astronautics And Aeronautics


Progress In Astronautics And Aeronautics
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Author :
language : en
Publisher:
Release Date : 1963

Progress In Astronautics And Aeronautics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aeronautics categories.




Internal Combustion Processes Of Liquid Rocket Engines


Internal Combustion Processes Of Liquid Rocket Engines
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Author : Zhen-Guo Wang
language : en
Publisher: John Wiley & Sons
Release Date : 2016-05-17

Internal Combustion Processes Of Liquid Rocket Engines written by Zhen-Guo Wang and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2016-05-17 with Technology & Engineering categories.


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.