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Theory Of Combustion Instability In Liquid Propellant Rocket Motors
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Book Synopsis Liquid Propellant Rocket Combustion Instability by : David T. Harrje
Download or read book Liquid Propellant Rocket Combustion Instability written by David T. Harrje and published by . This book was released on 1972 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Theory of Combustion Instability in Liquid Propellant Rocket Motors by : Luigi CROCCO (and CHENG (Sin-I))
Download or read book Theory of Combustion Instability in Liquid Propellant Rocket Motors written by Luigi CROCCO (and CHENG (Sin-I)) and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theory of Combustion Instability in Liquid Propellant Rocket Motors by : Luigi Crocco
Download or read book Theory of Combustion Instability in Liquid Propellant Rocket Motors written by Luigi Crocco and published by . This book was released on 1956 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents a theoretical analysis of combustion instability in liquid rocket motors.
Book Synopsis Liquid Rocket Engine Combustion Instability by : Vigor Young
Download or read book Liquid Rocket Engine Combustion Instability written by Vigor Young and published by AIAA. This book was released on 1995 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Liquid Propellant Rocket Combustion Instability by :
Download or read book Liquid Propellant Rocket Combustion Instability written by and published by . This book was released on 1972 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Mark L. Dranovsky Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9781563479212 Total Pages :352 pages Book Rating :4.4/5 (792 download)
Book Synopsis Combustion Instabilities in Liquid Rocket Engines by : Mark L. Dranovsky
Download or read book Combustion Instabilities in Liquid Rocket Engines written by Mark L. Dranovsky and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2007 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors by : Ben T. Zinn
Download or read book A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket Motors written by Ben T. Zinn and published by . This book was released on 1966 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Internal Combustion Processes of Liquid Rocket Engines by : Zhen-Guo Wang
Download or read book Internal Combustion Processes of Liquid Rocket Engines written by Zhen-Guo Wang and published by John Wiley & Sons. This book was released on 2016-05-17 with total page 509 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors by : David T. Harrje
Download or read book Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors written by David T. Harrje and published by . This book was released on 1964 with total page 205 pages. Available in PDF, EPUB and Kindle. Book excerpt: Topics include: Nonlinear theoretical approaches - longitudinal and transverse modes (calculations based on the nonlinear longitudinal mode with time-lag effects, a shock wave model of unstable rocket combustors with small time-lag effects, transverse nozzle admittance relation for finite-amplitude waves); Nonlinear combustion instability mechanisms (transverse mode nonlinear rocket motor studies, longitudinal nonlinear rocket studies using the square-motor, vapor displacement mechanism - basic experiment in the pseudo rocket, basic experiments in droplet resonant phenomena); Droplet and wake burning - mechanism for combustion instability; High subsonic mach number extensions to the linearized theory; Expressions for transverse waves; Concept in rocket baffle design.
Book Synopsis THEORY OF COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET MO by :
Download or read book THEORY OF COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET MO written by and published by . This book was released on with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Proceedings of the ... Interagency Chemical Rocket Propulsion Combustion Instability Conference by :
Download or read book Proceedings of the ... Interagency Chemical Rocket Propulsion Combustion Instability Conference written by and published by . This book was released on 1967 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Fundamentals of Acoustic Instabilities in Liquid Propellant Rockets by :
Download or read book Fundamentals of Acoustic Instabilities in Liquid Propellant Rockets written by and published by . This book was released on 1992 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this program, equations were written describing combustion instability in liquid-propellant rocket motors. The nonhomogeneous nature of the acoustic medium was taken into account, with the possibility of both subcritical and supercritical bifurcations occurring in the liquid-gas system. Attention was focused on characteristic times of the various flow, mixing and combustion processes as they arise in the newer engines of interest to the Air Force, in an effort to identify important physical phenomena in the instability and to achieve tractable descriptions of the instability processes. Theory was compared with available experimental observations in an effort to evaluate current theoretical capabilities. Combustion instability, Liquid-propellant rockets.
Book Synopsis Liquid Propellant Rocket Combustion Instability by : David T. Harrje
Download or read book Liquid Propellant Rocket Combustion Instability written by David T. Harrje and published by . This book was released on 1972 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Combustion Instability in Liquid Propellant Rocket Motors by :
Download or read book Combustion Instability in Liquid Propellant Rocket Motors written by and published by . This book was released on 1955 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Combustion Processes and Instabilities in Liquid-Propellant Rocket Engines by :
Download or read book Combustion Processes and Instabilities in Liquid-Propellant Rocket Engines written by and published by . This book was released on 2004 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research was directed towards developing new knowledge of combustion processes in liquid-propellant rocket engines. Attention was given to the combustion of different fuels, beginning with hydrogen-oxygen but ultimately including multicomponent hydrocarbon mixtures representative of RP fuels, and to nonlinear processes of importance in combustion instability. Effects of detailed chemical kinetics on performance and stability were addressed by introducing systematically reduced chemistry that enables theoretical analysis to be completed thoroughly and accurately. The interactions between chemistry and turbulence were addressed, including the effects of the heat release on the turbulence. The orientation of the work was fundamental and aimed at predicting not only performance and acoustic response but also intrinsic instability. The results were intended to help to improve understanding of combustion mechanisms and combustion instabilities in liquid-propellant rocket motors. The most recent specific results concern induction times in hydrogen-oxygen mixtures and heal-release effects on turbulent missing.
Book Synopsis Combustion Instability in Liquid Propellant Rocket Engines by : Vito D. Agosta
Download or read book Combustion Instability in Liquid Propellant Rocket Engines written by Vito D. Agosta and published by . This book was released on 1966 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investigation is concerned with the development of a theoretical model for combustion instability, in the longitudinal mode, occurring in liquid propellant rocket engines that are employed in current practice. Experimental results are used both to help generate realistic physical models for combustion-wave phenomena in heterogeneously reacting systems, and for subsequent verification of theoretical results. (Author).
Book Synopsis Fundamental Concepts of Liquid-Propellant Rocket Engines by : Alessandro de Iaco Veris
Download or read book Fundamental Concepts of Liquid-Propellant Rocket Engines written by Alessandro de Iaco Veris and published by Springer Nature. This book was released on 2020-09-26 with total page 747 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
