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Author : Martin Hersch
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (249 download)
Download or read book A Mixing Model for Rocket Engine Combustion written by Martin Hersch and published by . This book was released on 1965 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Martin Hersch
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Mixing Model for Rocket Engine Combustion written by Martin Hersch and published by . This book was released on 1965 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Zhen-Guo Wang
Publisher : John Wiley & Sons
ISBN 13 : 1118890051
Total Pages : 509 pages
Book Rating : 4.1/5 (188 download)
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.
Author : DP Mishra
Publisher : CRC Press
ISBN 13 : 1351708414
Total Pages : 364 pages
Book Rating : 4.3/5 (517 download)
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Author : David T. Harrje
Publisher :
ISBN 13 :
Total Pages : 668 pages
Book Rating : 4.:/5 (31 download)
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.
Author :
Publisher :
ISBN 13 :
Total Pages : 674 pages
Book Rating : 4.3/5 (91 download)
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : P. T. Hinde
Publisher :
ISBN 13 :
Total Pages : 55 pages
Book Rating : 4.:/5 (11 download)
Download or read book Basic Aspects of Gas-phase Mixing and Kinetics in Rocket Engine Combustion Chambers written by P. T. Hinde and published by . This book was released on 1969 with total page 55 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)
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.
Author : W. H. Sargent
Publisher :
ISBN 13 :
Total Pages : 123 pages
Book Rating : 4.:/5 (227 download)
Download or read book Investigation of Air-Augmented Rocket Combustion and Mixing Processes written by W. H. Sargent and published by . This book was released on 1967 with total page 123 pages. Available in PDF, EPUB and Kindle. Book excerpt: Data on coaxial jet mixing and combustion developed during a ten-week test program are presented along with a limited analysis of results. The test was conducted with a rocket motor simulator which generated a fuel-rich primary stream. The combustion of the primary stream was varied systematically through a broad range of conditions, and the exchange processes were observed in a secondary mixing duct by means of wall pressure measurements, thrust measurements, and measurements of heat flux. Photographic observations were made of the primary stream operating as a free jet. Preliminary analysis indicates that the length of duct required for momentum and energy exchange to occur depends primarily upon the secondary air mass flow. A brief discussion is included on the grouping of variables in afterburning problems, and a simplified 'throttling number' parameter is suggested. Also included are the results of a mixing zone computation in which the differential equations of coaxial mixing are solved by a finite difference procedure. Results are presented of calculations made to predict wall pressure profiles that are influenced by the presence of the bluff face of the primary stream blast tube. This analysis covers the flow regime that extends to the length of the primary stream potential core. (Author).
Author : John R. Szuch
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)
Download or read book Digital Computer Program for Analysis of Chugging Instabilities written by John R. Szuch and published by . This book was released on 1970 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 442 pages
Book Rating : 4.0/5 ( download)
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1966 with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Chin-Lung Chuang
Publisher :
ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.:/5 (273 download)
Download or read book Experimental Study of Mixing and Combustion Processes in a Solid-propellant Ducted Rocket Motor written by Chin-Lung Chuang and published by . This book was released on 1989 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Andrzej Dobrowolski
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (31 download)
Download or read book Analysis of Nonconstant Area Combustion and Mixing in Ramjet and Rocket-ramjet Hybrid Engines written by Andrzej Dobrowolski and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Leon V. Feigenbutz
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (227 download)
Download or read book Turbulent Mixing and Combustion of a Rocket Exhaust Jet with the Surrounding Atmosphere. Part I. the Balanced Jet written by Leon V. Feigenbutz and published by . This book was released on 1962 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flow field for a free jet, burning with the surrounding atmosphere, was calculated. The calculations were carried out for two different cases. In the first case, a rocket engine whose exit pressure is balanced with the ambient pressure of the standard atmosphere of 15,500 ft. is considered. In the second, a rocket engine whose exit pressure is balanced with the ambient pressure of the standard atmosphere at an altitude of 50,000 ft. is considered. (Author).
Author : Michał Lunc
Publisher : Elsevier
ISBN 13 : 1483184323
Total Pages : 613 pages
Book Rating : 4.4/5 (831 download)
Download or read book Propulsion Re-Entry Physics written by Michał Lunc and published by Elsevier. This book was released on 2014-05-09 with total page 613 pages. Available in PDF, EPUB and Kindle. Book excerpt: Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.
Author : Oak Ridge National Laboratory
Publisher :
ISBN 13 :
Total Pages : 1296 pages
Book Rating : 4.:/5 (31 download)
Download or read book Inventory of Current Energy Research and Development written by Oak Ridge National Laboratory and published by . This book was released on 1972 with total page 1296 pages. Available in PDF, EPUB and Kindle. Book excerpt:
