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Монографія на здобуття наукового ступеня доктора технічних наук за спеціальністю 05.05.03 – Двигуни та енергетичні установки. – Національ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3033::f8ddd8369b3e0b8f2a0519641087d453
http://repository.kpi.kharkov.ua/handle/KhPI-Press/50440
http://repository.kpi.kharkov.ua/handle/KhPI-Press/50440
Publikováno v:
Наукові вісті НТУУ «КПІ»: науково-технічний журнал
Досліджено та математично змодельовано процес теплообміну в циліндрі стаціонарного газового двигуна з форкамерно-факельним запалюван
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2635::49222dfc592464c44ecdbfccc0a1caf5
https://ela.kpi.ua/handle/123456789/14456
https://ela.kpi.ua/handle/123456789/14456
Autor:
Wang, Le
The ingestion of hot mainstream gas into the wheel-space between the rotor and staler discs is one of the most important internal cooling problems for gas turbine designers. To solve this problem, engineers design a rim seal at the periphery of wheel
Externí odkaz:
https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894
Publikováno v:
Eastern-European Journal of Enterprise Technologies; Том 3, № 10(51) (2011): Modern technologies in gas-turbine construction; 37-43
Восточно-Европейский журнал передовых технологий; Том 3, № 10(51) (2011): Современные технологии в газотурбостроении; 37-43
Східно-Європейський журнал передових технологій; Том 3, № 10(51) (2011): Сучасні технології в газотурбобудуванні; 37-43
Восточно-Европейский журнал передовых технологий; Том 3, № 10(51) (2011): Современные технологии в газотурбостроении; 37-43
Східно-Європейський журнал передових технологій; Том 3, № 10(51) (2011): Сучасні технології в газотурбобудуванні; 37-43
A standardized range of regenerative gas turbogenerators (GTG) for ship’s and stationary application with capacity 600-1,900 KW was offered
Унифицированный ряд регенеративных газотурбогенератор
Унифицированный ряд регенеративных газотурбогенератор
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=scientific_p::6114392897e06e07387e5eb439de1f1f
http://journals.uran.ua/eejet/article/view/1702
http://journals.uran.ua/eejet/article/view/1702
Autor:
Oguntade, Habeeb Idowu
This thesis presents CFD predictions of gas turbine film and effusion cooling. The dearth of detailed experimental adiabatic effusion cooling data led to the validation of the computational procedures against the experimental adiabatic cooling effect
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.581946
Autor:
Luque Martínez, Salvador G.
A novel experimental facility for the testing of modern high pressure nozzle guide vanes, the Annular Sector Heat Transfer Facility, is described in this thesis. Non- dimensionally similar conditions to a thermal paint test are reproduced, in a warm
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.558543
Autor:
Gunasekaran, Barani
Combustion instabilities (thermo-acoustic pressure oscillations) have been recognised for some time as a problem limiting the development of low emissions (e.g., lean burn) gas turbine combustion systems, particularly for aviation propulsion applicat
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.554111
Autor:
Yaqub, Sarmad
The experimental investigation of the combustion dynamics in a full scale industrial gas turbine combustor has been conducted. The successful capture of different combustion observables; including chemiluminescence emissions from C2* and CH* radicals
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.488996
Autor:
Gill, Christopher Mark
Near surface compressive residual stresses are known to improve the fatigue performance and damage tolerance of materials. In the aerospace gas turbine industry there is a compressive residual stress fields to extend the safe life time of a component
Externí odkaz:
http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494605