000447857 000__ 02862cam\a2200445\a\4500 000447857 001__ 447857 000447857 005__ 20210513154732.0 000447857 006__ m\\\\\\\\d\\\\\\\\ 000447857 007__ cr\cn||||||||| 000447857 008__ 101023s2007\\\\vaua\\\\sb\\\\001\0\eng\d 000447857 010__ $$z 2010501922 000447857 020__ $$z1563479214 000447857 020__ $$z9781563479212 000447857 020__ $$z9781600864711 (e-book) 000447857 035__ $$a(CaPaEBR)ebr10516675 000447857 035__ $$a(OCoLC)774285720 000447857 040__ $$aCaPaEBR$$cCaPaEBR 000447857 043__ $$ae-ur--- 000447857 05014 $$aTL783.4$$b.D73 2007eb 000447857 08204 $$a621.43/56$$223 000447857 1001_ $$aDranovsky, Mark L. 000447857 24510 $$aCombustion instabilities in liquid rocket engines$$h[electronic resource] :$$btesting and development practices in Russia /$$cMark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley. 000447857 260__ $$aReston, Va. :$$bAmerican Institute of Aeronautics and Astronautics,$$cc2007. 000447857 300__ $$axix, 321 p. :$$bill. 000447857 4901_ $$aProgress in astronautics and aeronautics ;$$vv. 221 000447857 504__ $$aIncludes bibliographical references and index. 000447857 5050_ $$aIntroduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. 000447857 506__ $$aAccess limited to authorized users. 000447857 650_0 $$aLiquid propellant rockets. 000447857 650_0 $$aRocket engines$$xCombustion$$zRussia (Federation)$$xTesting. 000447857 650_0 $$aLiquid fuels$$xCombustion$$zRussia (Federation)$$xTesting. 000447857 650_0 $$aRockets (Aeronautics)$$zRussia (Federation)$$xTesting. 000447857 655_7 $$aElectronic books.$$2lcsh 000447857 7001_ $$aYang, Vigor. 000447857 7001_ $$aCulick, F.$$q(Fred),$$d1933- 000447857 7001_ $$aTalley, Douglas G. 000447857 830_0 $$aProgress in astronautics and aeronautics. 000447857 852__ $$bebk 000447857 85640 $$3ProQuest Ebook Central Academic Complete$$uhttps://univsouthin.idm.oclc.org/login?url=http://site.ebrary.com/lib/usiricelib/Doc?id=10516675$$zOnline Access 000447857 909CO $$ooai:library.usi.edu:447857$$pGLOBAL_SET 000447857 980__ $$aEBOOK 000447857 980__ $$aBIB 000447857 982__ $$aEbook 000447857 983__ $$aOnline