.

0 (hodnocen0 x )

EB

ONLINE

Reston, Va. : American Institute of Aeronautics and Astronautics, c2007

1 online resource (xix, 321 p.) : ill

ISBN 9781600864711 (electronic bk.)

ISBN 1563479214

ISBN 9781563479212

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

001807800

full

(Au-PeEL)EBL3111571

(CaPaEBR)ebr10516675

(MiAaPQ)EBC3111571

(OCoLC)922978803