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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



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Autore: Dranovsky Mark L Visualizza persona
Titolo: 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 Visualizza cluster
Pubblicazione: Reston, Va., : American Institute of Aeronautics and Astronautics, c2007
Descrizione fisica: 1 online resource (342 p.)
Disciplina: 621.43/56
Soggetto topico: Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing
Liquid fuels - Combustion - Russia (Federation) - Testing
Rockets (Aeronautics) - Russia (Federation) - Testing
Altri autori: YangVigor  
CulickF <1933-> (Fred)  
TalleyDouglas G  
Note generali: Description based upon print version of record.
Nota di bibliografia: Includes bibliographical references and index.
Nota di contenuto: 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.
Titolo autorizzato: Combustion instabilities in liquid rocket engines  Visualizza cluster
ISBN: 1-60086-690-5
1-60086-471-6
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910817251603321
Lo trovi qui: Univ. Federico II
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Serie: Progress in astronautics and aeronautics.