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Liquid rocket engine combustion instability /
Annotation
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Washington, D.C. :
American Institute of Aeronautics and Astronautics,
1995.
|
| Colección: | Progress in astronautics and aeronautics ;
v. 169. |
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 037 | |a 3111646 |b Proquest Ebook Central | ||
| 050 | 4 | |a TL783.4 |b .L57 1995eb | |
| 082 | 0 | 4 | |a 629.47522 |
| 049 | |a UAMI | ||
| 245 | 0 | 0 | |a Liquid rocket engine combustion instability / |c edited by Vigor Yang. |
| 260 | |a Washington, D.C. : |b American Institute of Aeronautics and Astronautics, |c 1995. | ||
| 300 | |a 1 online resource (564 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Progress in astronautics and aeronautics ; |v v. 169 | |
| 504 | |a Includes bibliographical references and index. | ||
| 505 | 0 | |a pt. 1. Instability phenomenology and case studies -- pt. 2. Fundamental mechanisms of combustion instabilities -- pt. 3. Combustion instability analysis -- pt. 4. Stability testing methodology. | |
| 520 | 8 | |a Annotation |b 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. | |
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 650 | 0 | |a Liquid propellant rockets. | |
| 650 | 0 | |a Rocket engines |x Combustion. | |
| 650 | 6 | |a Fusées à propergol liquide. | |
| 650 | 6 | |a Moteurs-fusées |x Combustion. | |
| 650 | 7 | |a Liquid propellant rockets |2 fast | |
| 650 | 7 | |a Rocket engines |x Combustion |2 fast | |
| 700 | 1 | |a Young, Vigor. | |
| 776 | 0 | 8 | |i Print version: |a Young, Vigor. |t Liquid Rocket Engine Combustion Instability. |d Reston : American Institute of Aeronautics and Astronautics, ©2000 |z 9781563471834 |
| 830 | 0 | |a Progress in astronautics and aeronautics ; |v v. 169. | |
| 856 | 4 | 0 | |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111646 |z Texto completo |
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