Combustion instabilities in liquid rocket engines : testing and development practices in Russia /

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
:
ProQuest (Firm)
Dranovsky, Mark L.
TeilnehmendeR:
Yang, Vigor.
Culick, F. 1933-
Talley, Douglas G.
ProQuest (Firm)
Year of Publication:2007
Language:English
Series:Progress in astronautics and aeronautics.
Online Access:
Physical Description:xix, 321 p. :; ill.
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(Au-PeEL)EBL3111571
(CaPaEBR)ebr10516675
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collection bib_alma
record_format marc
spelling Dranovsky, Mark L.
Combustion instabilities in liquid rocket engines [electronic resource] : testing and development practices in Russia / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
Reston, Va. : American Institute of Aeronautics and Astronautics, c2007.
xix, 321 p. : ill.
Progress in astronautics and aeronautics ; v. 221
Includes bibliographical references and index.
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.
Electronic reproduction. Ann Arbor, MI : ProQuest, 2015. Available via World Wide Web. Access may be limited to ProQuest affiliated libraries.
Liquid propellant rockets.
Rocket engines Combustion Russia (Federation) Testing.
Liquid fuels Combustion Russia (Federation) Testing.
Rockets (Aeronautics) Russia (Federation) Testing.
Electronic books.
Yang, Vigor.
Culick, F. (Fred), 1933-
Talley, Douglas G.
ProQuest (Firm)
Progress in astronautics and aeronautics.
https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=3111571 Click to View
language English
format Electronic
eBook
author Dranovsky, Mark L.
spellingShingle Dranovsky, Mark L.
Combustion instabilities in liquid rocket engines testing and development practices in Russia /
Progress in astronautics and aeronautics ;
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.
author_facet Dranovsky, Mark L.
Yang, Vigor.
Culick, F. 1933-
Talley, Douglas G.
ProQuest (Firm)
ProQuest (Firm)
author_variant m l d ml mld
author2 Yang, Vigor.
Culick, F. 1933-
Talley, Douglas G.
ProQuest (Firm)
author2_variant v y vy
f c fc
d g t dg dgt
author2_fuller (Fred),
author2_role TeilnehmendeR
TeilnehmendeR
TeilnehmendeR
TeilnehmendeR
author_corporate ProQuest (Firm)
author_sort Dranovsky, Mark L.
title Combustion instabilities in liquid rocket engines testing and development practices in Russia /
title_sub testing and development practices in Russia /
title_full Combustion instabilities in liquid rocket engines [electronic resource] : testing and development practices in Russia / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
title_fullStr Combustion instabilities in liquid rocket engines [electronic resource] : testing and development practices in Russia / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
title_full_unstemmed Combustion instabilities in liquid rocket engines [electronic resource] : testing and development practices in Russia / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.
title_auth Combustion instabilities in liquid rocket engines testing and development practices in Russia /
title_new Combustion instabilities in liquid rocket engines
title_sort combustion instabilities in liquid rocket engines testing and development practices in russia /
series Progress in astronautics and aeronautics ;
series2 Progress in astronautics and aeronautics ;
publisher American Institute of Aeronautics and Astronautics,
publishDate 2007
physical xix, 321 p. : ill.
contents 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.
isbn 9781600864711 (electronic bk.)
callnumber-first T - Technology
callnumber-subject TL - Motor Vehicles and Aeronautics
callnumber-label TL783
callnumber-sort TL 3783.4 D73 42007
genre Electronic books.
genre_facet Electronic books.
geographic_facet Russia (Federation)
url https://ebookcentral.proquest.com/lib/oeawat/detail.action?docID=3111571
illustrated Illustrated
dewey-hundreds 600 - Technology
dewey-tens 620 - Engineering
dewey-ones 621 - Applied physics
dewey-full 621.43/56
dewey-sort 3621.43 256
dewey-raw 621.43/56
dewey-search 621.43/56
oclc_num 922978803
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is_hierarchy_title Combustion instabilities in liquid rocket engines testing and development practices in Russia /
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