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Combustion instability /
Annotation
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés Ruso |
| Publicado: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
©1999.
|
| Colección: | Progress in astronautics and aeronautics ;
v. 222. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Natanzon, M. S. |q (Miron Semenovich) | |
| 240 | 1 | 0 | |a Neustoĭchivostʹ gorenii͡a. |l English |
| 245 | 1 | 0 | |a Combustion instability / |c M.S. Natanzon ; edited by F.E.C. Culick. |
| 260 | |a Reston, Va. : |b American Institute of Aeronautics and Astronautics, |c ©1999. | ||
| 300 | |a 1 online resource (xxviii, 258 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
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| 490 | 1 | |a Progress in astronautics and aeronautics ; |v v. 222 | |
| 500 | |a Originally published in 1986 by Mashinostroenie, Moscow. | ||
| 504 | |a Includes bibliographical references (pages 245-249) and index. | ||
| 546 | |a Translated electronically in 1996; English translation revised by author. | ||
| 588 | 0 | |a Print version record. | |
| 505 | 0 | |a Low frequency oscillations in liquid rocket combustion chambers -- Phenomenological models of the combustion process -- The acoustic response of the combustion chamber -- High-frequency (acoustic) oscillations in a combustion chamber -- Nonlinear effects -- Application of the frequency-response method for studying the dynamical properties of the combustion zone -- Stability of combustion of fuel drops in a flow of gaseous oxidizer -- Bifurcations of steady combustion regimes and their effect on the onset of high-frequency oscillations. | |
| 520 | 8 | |a Annotation |b This book?much of it formerly classified material--is a clear exposition of much of the theoretical work on combustion instabilities, performed in support of the Soviet liquid rocket program during its most vigorous period. While there are similarities between Western and Eastern works, there are many distinct differences. The author was one of the small group of Soviet theorists actively engaged in all of the Soviet liquid rocket programs. His development of the field is firmly grounded in fundamental ideas, and progresses to applications of a general sort. One chapter is new since the original Russian edition, covering both theory and experiment for bifurcations of dynamical behavior in liquid rocket chambers. | |
| 590 | |a Knovel |b ACADEMIC - Aerospace & Radar Technology | ||
| 650 | 0 | |a Combustion. | |
| 650 | 6 | |a Combustion. | |
| 650 | 7 | |a combustion. |2 aat | |
| 650 | 7 | |a Combustion |2 fast | |
| 700 | 1 | |a Culick, F. |q (Fred), |d 1933- | |
| 776 | 0 | 8 | |i Print version: |a Natanzon, M.S. (Miron Semenovich). |s Neustoĭchivostʹ gorenii͡a. English. |t Combustion instability. |d Reston, Va. : American Institute of Aeronautics and Astronautics, ©1999 |z 1563479281 |w (OCoLC)177505379 |
| 830 | 0 | |a Progress in astronautics and aeronautics ; |v v. 222. | |
| 856 | 4 | 0 | |u https://appknovel.uam.elogim.com/kn/resources/kpCIPAAV01/toc |z Texto completo |
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