TY  - BOOK
AU  - Dranovsky,Mark L.
AU  - Yang,Vigor
AU  - Culick,F.
AU  - Talley,Douglas G.
ED  - ProQuest (Firm)
TI  - Combustion instabilities in liquid rocket engines: testing and development practices in Russia 
T2  - Progress in astronautics and aeronautics
AV  - TL783.4 .D73 2007
U1  - 621.43/56 23
PY  - 2007///
CY  - Reston, Va.
PB  - American Institute of Aeronautics and Astronautics
KW  - Liquid propellant rockets
KW  - Rocket engines
KW  - Combustion
KW  - Russia (Federation)
KW  - Testing
KW  - Liquid fuels
KW  - Rockets (Aeronautics)
KW  - Electronic books
N1  - 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
UR  - https://ebookcentral.proquest.com/lib/bacm-ebooks/detail.action?docID=3111571
ER  -