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|a TL783.4
|b .D73 2007eb
|
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0 |
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|a 621.43/56
|2 23
|
| 049 |
|
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|a UAMI
|
| 100 |
1 |
|
|a Dranovsky, Mark L.
|
| 245 |
1 |
0 |
|a Combustion instabilities in liquid rocket engines :
|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 ©2007.
|
| 300 |
|
|
|a 1 online resource (xix, 321 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. 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.
|
| 590 |
|
|
|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 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.
|
| 650 |
|
6 |
|a Fusées à propergol liquide.
|
| 650 |
|
7 |
|a Liquid propellant rockets
|2 fast
|
| 650 |
|
7 |
|a Rockets (Aeronautics)
|x Testing
|2 fast
|
| 651 |
|
7 |
|a Russia (Federation)
|2 fast
|1 https://id.oclc.org/worldcat/entity/E39PBJhhmCp3jtcMQbx3WgpXVC
|
| 655 |
|
7 |
|a dissertations.
|2 aat
|
| 655 |
|
7 |
|a Academic theses
|2 fast
|
| 655 |
|
7 |
|a Academic theses.
|2 lcgft
|
| 655 |
|
7 |
|a Thèses et écrits académiques.
|2 rvmgf
|
| 700 |
1 |
|
|a Yang, Vigor.
|
| 700 |
1 |
|
|a Culick, F.
|q (Fred),
|d 1933-
|1 https://id.oclc.org/worldcat/entity/E39PCjwpwC6yjTXf9hcRFtPvVy
|
| 700 |
1 |
|
|a Talley, Douglas G.
|
| 776 |
0 |
8 |
|i Print version:
|a Dranovsky, Mark L.
|t Combustion instabilities in liquid rocket engines.
|d Reston, Va. : American Institute of Aeronautics and Astronautics, ©2007
|w (DLC) 2010501922
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111571
|z Texto completo
|
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