Tools

LEADER 03670cam a22005777a 4500

001 ssj0000551091;

003 WaSeSS;

005 20190313051101.0;

006 m d ;

007 cr n ;

008 101023s2007 vaua sb 001 0 eng d;

010 a| 2010501922;

015 a| GBA8075072| bnb;

016 7 a| 0144944682| Uk;

020 a| 9781563479212;

020 a| 1563479214;

035 a| (WaSeSS)ssj0000551091;

042 a| pcc;

043 a| e-ur---;

049 a| EREEa| NEHH;

050 00 a| TL783.4b| .D73 2007;

082 00 a| 621.43/562| 23;

100 1 a| Dranovsky, Mark L.?| UNAUTHORIZED;

245 10 a| Combustion instabilities in liquid rocket enginesh| [electronic resource] :b| testing and development practices in Russia /c| Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley.;

260 a| Reston, Va. :b| American Institute of Aeronautics and Astronautics,;

300 a| xix, 321 p. :b| ill. ;c| 24 cm.;

490 1 a| Progress in astronautics and aeronautics ;v| v. 221;

504 a| Includes bibliographical references (p. 309-314) and index.;

505 0 a| 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.;

506 a| Available only to authorized users.;

538 a| Mode of access: World Wide Web;

650 0 a| Liquid propellant rockets.=| ^A220003;

650 0 a| Rockets (Aeronautics)z| Russia (Federation)x| Testing.=| ^A69864;

655 0 a| Electronic books.=| ^A491897;

700 1 a| Yang, Vigor.=| ^A1011760;

700 1 a| Culick, F.q| (Fred),d| 1933-=| ^A566673;

700 1 a| Talley, Douglas G.?| UNAUTHORIZED;

830 0 a| Progress in astronautics and aeronautics.=| ^A674333;

856 40 z| Full text available from Ebook Central - Academic Completeu| https://ebookcentral.proquest.com/lib/eastcarolina/detail.action?docID=3111571;

947 a| (OCoLC)ocn166372980;

949 a| CLICK ON WEB ADDRESSw| ASISh| JOYNER188;

949 a| CLICK ON WEB ADDRESSw| ASISh| HSL77;

949 a| CLICK ON WEB ADDRESSw| ASISh| JMUSIC60;

596 a| 1 3 4;

998 a| 4019667;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4019667-1001l| JNETm| JOYNERr| Ys| Yt| JNESSBKu| 1/1/2016x| EBOOKz| JERESOURCE;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4019667-2001l| HSLELECm| HSLr| Ys| Yt| HEBKu| 1/1/2016x| EBOOKz| HERESOURCE;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4019667-3001l| MNETm| JMUSICr| Ys| Yt| MNESSBKu| 1/1/2016x| EBOOKz| JERESOURCE;

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.

Author/creator	Dranovsky, Mark L.
Other author	Yang, Vigor.
Other author	Culick, F. (Fred), 1933-
Other author	Talley, Douglas G.
Format	Electronic
Publication Info	Reston, Va. : American Institute of Aeronautics and Astronautics,
Description	xix, 321 p. : ill. ; 24 cm.
Supplemental Content	Full text available from Ebook Central - Academic Complete
Subjects	Liquid propellant rockets. Rocket engines--Combustion. --Russia (Federation). --Testing. Liquid fuels--Combustion. --Russia (Federation). --Testing. Rockets (Aeronautics)--Russia (Federation). --Testing.

Series	Progress in astronautics and aeronautics ; v. 221 Progress in astronautics and aeronautics. ^A674333
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.
Bibliography note	Includes bibliographical references (p. 309-314) and index.
Access restriction	Available only to authorized users.
Technical details	Mode of access: World Wide Web
Genre/form	Electronic books.
LCCN	2010501922
ISBN	9781563479212
ISBN	1563479214

Availability

Library	Location	Call Number	Status	Item Actions
	Electronic Resources	Access Content Online	✔ Available

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.

Click here for more information about this title

Availability