Numerical Analysis Of Liquid Rocket Engine Combustion Instability
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Numerical Analysis Of Liquid Rocket Engine Combustion Instability
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Author : I. Dubois
language : en
Publisher:
Release Date : 1995
Numerical Analysis Of Liquid Rocket Engine Combustion Instability written by I. Dubois and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with categories.
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 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.
Numerical Analysis Of Combustion Instability In Liquid Propellant Rocket Engine
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Author : Weidong Liu
language : en
Publisher:
Release Date : 1995
Numerical Analysis Of Combustion Instability In Liquid Propellant Rocket Engine written by Weidong Liu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with categories.
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.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Advanced Technologies In Flow Dynamics And Combustion In Propulsion And Power
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Author : Lei Luo
language : en
Publisher: Frontiers Media SA
Release Date : 2022-08-05
Advanced Technologies In Flow Dynamics And Combustion In Propulsion And Power written by Lei Luo and has been published by Frontiers Media SA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2022-08-05 with Technology & Engineering categories.
Performance Analysis Of A Liquid Gel Rocket Engine During Operation
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Author : Minchao Huang
language : en
Publisher: Springer Nature
Release Date : 2024-10-01
Performance Analysis Of A Liquid Gel Rocket Engine During Operation written by Minchao Huang and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2024-10-01 with Technology & Engineering categories.
This open access book takes space propulsion system, gel propulsion system, and pumped liquid rocket engine as research objects and establishes and describes the theory, dynamic model, and numerical calculation method of working process of liquid/gel rocket engine. The first part of this book establishes a mathematical model for the working process of the space propulsion system, including a mathematical model for gas cylinders, an electric explosion valve, a pressure reducing valve, a storage tank, a liquid pipeline, an orifice and filter, an electromagnetic valve, a filling pipeline, and a thrust chamber. The simulation analyzes the characteristics of the start-up, steady-state, and shutdown processes of the space propulsion system. In the second part, the mathematical model of the working process of gel propulsion system is established, and the flow distribution law, water hammer characteristics, and thrust regulation characteristics of gel propulsion system are simulated and analyzed. The third part establishes a mathematical model for the working process of a pumped liquid rocket engine and simulates and analyzes the starting process characteristics of the pumped liquid rocket engine. The above theory or dynamic model reflects the latest research results of the working process of liquid/gel rocket engine. This book is used as a teaching material or reference book for teachers, students, and scientific and technological personnel engaged in the simulation analysis of the working process of liquid/gel rocket engines in the fields of aerospace, aviation, power, etc.
41st Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 10 13 July 2005 Tucson Arizona 05 3700 05 3749
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Author :
language : en
Publisher:
Release Date : 2005
41st Aiaa Asme Sae Asee Joint Propulsion Conference Exhibit 10 13 July 2005 Tucson Arizona 05 3700 05 3749 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Airplanes categories.
Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1963
Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Science categories.