Combustion instabilities in liquid rocket engines testing and development practices in Russia /
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| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | , , |
| Format: | Electronic eBook |
| Language: | English |
| Published: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
c2007.
|
| Series: | Progress in astronautics and aeronautics.
|
| Subjects: | |
| Online Access: | An electronic book accessible through the World Wide Web; click to view |
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| 020 | |z 9781563479212 | ||
| 020 | |z 9781600864711 (e-book) | ||
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| 082 | 0 | 4 | |a 621.43/56 |2 23 |
| 100 | 1 | |a Dranovsky, Mark L. | |
| 245 | 1 | 0 | |a Combustion instabilities in liquid rocket engines |h [electronic resource] : |b testing and development practices in Russia / |c Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley. |
| 260 | |a Reston, Va. : |b American Institute of Aeronautics and Astronautics, |c c2007. | ||
| 300 | |a xix, 321 p. : |b ill. | ||
| 490 | 1 | |a Progress in astronautics and aeronautics ; |v v. 221 | |
| 504 | |a Includes bibliographical references and index. | ||
| 505 | 0 | |a Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. | |
| 533 | |a Electronic reproduction. |b Palo Alto, Calif. : |c ebrary, |d 2012. |n Available via World Wide Web. |n Access may be limited to ebrary affiliated libraries. | ||
| 650 | 0 | |a Liquid propellant rockets. | |
| 650 | 0 | |a Rocket engines |x Combustion |z Russia (Federation) |x Testing. | |
| 650 | 0 | |a Liquid fuels |x Combustion |z Russia (Federation) |x Testing. | |
| 650 | 0 | |a Rockets (Aeronautics) |z Russia (Federation) |x Testing. | |
| 655 | 7 | |a Electronic books. |2 local | |
| 700 | 1 | |a Yang, Vigor. | |
| 700 | 1 | |a Culick, F. |q (Fred), |d 1933- | |
| 700 | 1 | |a Talley, Douglas G. | |
| 710 | 2 | |a ebrary, Inc. | |
| 830 | 0 | |a Progress in astronautics and aeronautics. | |
| 856 | 4 | 0 | |u http://site.ebrary.com/lib/daystar/Doc?id=10516675 |z An electronic book accessible through the World Wide Web; click to view |
| 908 | |a 170314 | ||
| 942 | 0 | 0 | |c EB |
| 999 | |c 132024 |d 132024 | ||