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| Author | : George Sotter |
| Publisher | : |
| Total Pages | : |
| Release | : 1962 |
| Genre | : |
| ISBN | : |
| Author | : J. Swithenbank |
| Publisher | : |
| Total Pages | : 173 |
| Release | : 1969 |
| Genre | : |
| ISBN | : |
| Author | : Vigor Young |
| Publisher | : AIAA |
| Total Pages | : 606 |
| Release | : 1995 |
| Genre | : Liquid propellant rockets |
| ISBN | : 9781600864186 |
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.
| Author | : Martin Summerfield |
| Publisher | : Elsevier |
| Total Pages | : 713 |
| Release | : 2013-11-11 |
| Genre | : Science |
| ISBN | : 0323163351 |
Solid Propellant Rocket Research
| Author | : Ben T. Zinn |
| Publisher | : |
| Total Pages | : |
| Release | : 1975 |
| Genre | : Combustion |
| ISBN | : |
| Author | : IIT RESEARCH INST CHICAGO ILL. |
| Publisher | : |
| Total Pages | : 9 |
| Release | : 1963 |
| Genre | : |
| ISBN | : |
Progress is reported on studies concerning the use of a fluid dynamic model for the combustion zone of a solid propellant rocket undergoing erosive burning. Work involved the debugging of a computer program, trial calculations using the program, and a study of the gas-phase reaction kinetics involved in nitrocellulosenitroglycerin combustion.
| Author | : Luigi De Luca |
| Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
| Total Pages | : 924 |
| Release | : 1992 |
| Genre | : Technology & Engineering |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 41 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
| Author | : D. E. Kooker |
| Publisher | : |
| Total Pages | : 183 |
| Release | : 1974 |
| Genre | : |
| ISBN | : |
Nonlinear axial-mode combustion instability remains a serious problem in the development of solid propellant rocket motors. Although the use of metal-loaded solid propellants which produce solid particles in the flow has reduced the occurrence of high frequency instabilities, it has not eliminated the axial-mode intermediate frequency (100 - 1000 Hz.) problem. If such an instability reaches a large amplitude limit cycle, it may lead to an increase in mean chamber pressure and burning rate, excessive heat transfer rates, and a severe vibration level. The objective of this report is to investigate the complex coupling between the chamber flow conditions and the solid propellant combustion process which may lead to large amplitude longitudinal instabilities. (Modified author abstract).
| Author | : Joseph D. Baum |
| Publisher | : |
| Total Pages | : 299 |
| Release | : 1984 |
| Genre | : |
| ISBN | : |
The investigation sought to further our understanding of the physical mechanisms which control the initiation and severity of nonlinear combustion instability in solid propellant rocket motors. It was directed towards understanding those mechanisms which influence the triggering of instabilities.
