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О.В. Короткая

12

Инженерный журнал: наука и инновации

# 12·2016

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Cheng Cheng, Yibai Wang, Yu Liu, Dawei Liu, Xingyu Lu Thermal-structural

response and low-cycle fatigue damage of channel wall nozzle.

Chinese Jour-

nal of Aeronautics

, 2013. Available at:

http://dx.doi.org/10.1016/j.cja.2013.07.045

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Korotkaya O.V. Termoprochnostnoy raschet soplovoy chasti ZhRD s ispol-

zovaniem metoda podkonstruktsii [Thermal-stress analysis and strength calcu-

lation of nozzle end of liquid-propellant rocket engine with the use of substruc-

ture method].

Sb. tr. Mezhdunar. konkursa nauchnykh rabot po prioritetnym

napravleniyam razvitiya nauki, tekhnologii i tekhniki v Rossiyskoy Federatsii

[International Science Project Competition. Collected papers]. Moscow, NII

elektroniki i lazernoytekhniki Publ., 2012, pp. 263–269.

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Gavryushin S.S., Krasnovskiy E.E., Korotkaya O.V., Strizhenko P.P., Katkov R.E.

Inzhenernyi zhurnal: nauka i innovatsii — Engineering Journal: Science and Inno-

vation

, 2013, no. 4. Available at:

http://engjournal.ru/catalog/machin/rocket/705.html

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Korotkaya O.V., Gavryushin S.S. Raschet kamery sgoraniya perspektivnogo

ZhRD na osnove metoda podkonstruktsii [Strength calculation of combustion

chamber of a perspective liquid-propellant rocket engine by using the substruc-

ture method].

Materialy XX Mezhdunar. simp. “Dinamicheskie i tekhnolo-

gicheskie problemy mekhaniki konstruktsiy i sploshnykh sred“ im. A.G. Gorshko-

va. T. 1

[XX International symposium “Dynamic and technological problems of a

mechanics of constructions and continua”. Collected papers. Vol. 1]. Moscow,

TR-print Ltd Publ., 2014, pp. 50–52.



Korotkaya O.V., Gavryushin S.S. Raschet kamery sgoraniya ZhRD s kislorodnym

okhlazhdeniem na osnove metoda podkonstruktsii [Analysis of a LOX-cooled

combustion chamber of a liquid-propellant rocket engine by using the substructure

method].

Materialy XXI Mezhdunar. simp. “Dinamicheskie i tekhnologicheskie

problemy mekhaniki konstruktsiy i sploshnykh sred“ im. A.G. Gorshkova. T. 1

[XXI International symposium “Dynamic and technological problems of a mechan-

ics of constructions and continua”. Collected papers. Vol. 1]. Moscow, TR-print

Ltd Publ., 2015, pp. 50–52.



Gavryushin S.S., Korotkaya O.V., Yagodnikov D.A., Polyanskiy A.R. Raschet

i proektirovanie kamery sgoraniya perspektivnogo ZhRD na osnove metoda

podkonstruktsii [Calculation and designing of combustion chamber of a per-

spective liquid-propellant rocket engine by using the substructure method].

Raketnye dvigateli i energeticheskie ustanovki: materialy dokl. Vseros. nauch.-

tekhn. konf., posviasch. 70-letiyu osnovaniya kafedry raketnykh dvigatelei Ka-

zanskogo aviatsionnogo instituta

[All-Russian Scientific Conference dedicated

to the 70th anniversary of the Department of rocket engines of Kazan Aviation

Institute. Collected papers]. Kazan, Kazan Aviation Institute Publ., 2015,

pp. 149–152.



Korotkaya O.V., Gavryushin S.S. Termoprochnostnoy raschet soplovoy chasti

kamery sgoraniya perspektivnogo zhidkostnogo raketnogo dvigatelya s kislo-

rodnym okhlazhdeniem s ispolzovaniem metoda podmodeley dlya optimizatsii

finansirovaniya pri sozdanii novykh ZhRD [Thermal-stress analysis of a com-

bustion chamber of a perspective LOX-cooled liquid propellant rocket engine

with the use of a submodeling method to optimize the financing while creating

new liquid propellant rocket engines].

Sb. materialov Vseros. nauch.-tekhn.

konf. “Raketno-kosmicheskie dvigatelnye ustanovki”, posvyashch. 90-letiyu so

dnya rozhdeniya Zasluzhennykh deyatelei nauki i tekhniki RF, laureatov Gosu-

darstvennoi premii SSSR, professorov Kudryavtseva V.M. i Polyaeva V.M.

i 185-letiyu MGTU im. N.E. Baumana

[All-Russian Scientific Conference