Combustion instabilities in liquid rocket engines : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
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| Superior document: | Progress in astronautics and aeronautics ; v. 221 |
|---|---|
| : | |
| TeilnehmendeR: | |
| Year of Publication: | 2007 |
| Language: | English |
| Series: | Progress in astronautics and aeronautics.
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| Online Access: | |
| Physical Description: | xix, 321 p. :; ill. |
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| 020 | |z 9781563479212 | ||
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| 050 | 4 | |a TL783.4 |b .D73 2007 | |
| 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. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest 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 | 4 | |a Electronic books. | |
| 700 | 1 | |a Yang, Vigor. | |
| 700 | 1 | |a Culick, F. |q (Fred), |d 1933- | |
| 700 | 1 | |a Talley, Douglas G. | |
| 710 | 2 | |a ProQuest (Firm) | |
| 830 | 0 | |a Progress in astronautics and aeronautics. | |
| 856 | 4 | 0 | |u https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=3111571 |z Click to View |