Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2013. – ¹ 8(105). – 294 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 8(105). –
294ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 8(105). – 294 ñ.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Æóëàé Þ.À., |
HYDRODYNAMIC
CAVITATION AS A TOOL TO INTENSIFY PRODUCTION PROCESSES. XPERIENCE OF USAGE
AND PROSPECTS (REVIEW) |
ÊÀ²ÒÀÖ²ß ßÊ ÇÀѲÁ
²ÍÒÅÍÑÈÔ²ÊÀÖ²¯ ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲÂ. ÄÎÑÂ²Ä ÇÀÑÒÎÑÓÂÀÍÍß É ÏÅÐÑÏÅÊÒÈÂÈ (ÎÃËßÄ) |
7–15 |
|
Íàáîêèíà Ò.Ï., |
INCREASE OF TECHNOLOGICAL
EQUIPMENT CLEANING EFFICIENCY OF thermogas dynamic METHOD AT PRODUCTION OF
GTÅ SHOULDER-BLADES |
²ÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² Î×ÈÙÅÍÍß
ÒÅÕÍÎËÎò×ÍÎÃÎ ÎÁËÀÄÍÀÍÍß ÒÅÐÌÎÃÀÇÎÄÈÍÀ̲×ÍÈÌ ÌÅÒÎÄÎÌ ÏÐÈ ÂÈÐÎÁÍÈÖÒ² ËÎÏÀÒÎÊ
ÃÒÄ |
16–20 |
|
Êëèìåíêî Ë.Ï., |
THERMO-INSULATION
COVERAGES OF WORKING SURFACE OF POROUS CASTING FORMS ARE FOR CASTING OF
SHELLS OF CYLINDERS OF ENGI |
ÒÅÐÌβÇÎËßÖ²ÉͲ
ÏÎÊÐÈÒÒß ÐÎÁÎ×ί ÏÎÂÅÐÕͲ ÏÎÐÈÑÒÈÕ ËÈÂÀÐÍÈÕ ÊÎʲ˲ ÄËß ËÈÒÒß Ã²ËÜÇ ÖÈ˲ÍÄвÂ
ÄÂÇ |
ÒÅÐÌÎÈÇÎËßÖÈÎÍÍÛÅ ÏÎÊÐÛÒÈß ÐÀÁÎ×ÅÉ
ÏÎÂÅÐÕÍÎÑÒÈ ÏÎÐÈÑÒÛÕ ËÈÒÅÉÍÛÕ ÊÎÊÈËÅÉ ÄËß ËÈÒÜß ÃÈËÜÇ ÖÈËÈÍÄÐÎÂ ÄÂÑ |
21–24 |
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Óëèòåíêî Þ.À., |
PROBLEMS OF
SELECTION OF CONFIGURATION FOR POWERPLANT INTENDED FOR SPACE TRANSPORTATION SYSTEM
STAGE 1 |
ÏðîáëåìÈ
âÈáîðÓ ñõåìÈ ñèëîâî¯ óñòàíîâêè äëÿ ÏÅÐØÎ¯ ñòóïåí² òðàíñïîðòíî-ÊÎÑ̲×Íί
ñèñòåìÈ |
ÏÐÎÁËÅÌÛ ÂÛÁÎÐÀ
ÑÕÅÌÛ ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÈ ÄËß ÏÅÐÂÎÉ ÑÒÓÏÅÍÈ ÒÐÀÍÑÏÎÐÒÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ |
25–30 |
Ïîâãîðîäíèé Â.Î. |
IDENTIFICATION
OF THE PARAMETER’S OF THERMOELASTICITY TO THE NONHOMOGENEOUS STRESS CONDITION
ON THE SOLUTION INVERSE PROBLEM OF THE THERMOELASTICITY |
²ÄÅÍÒÈÔ²ÊÀÖ²ß ÏÀÐÀÌÅÒвÂ
ÒÅÐÌÎÏÐÓÆÍÎÑÒ² ÒÎÍÊÎÑÒ²ÍÍÈÕ ÑÈÑÒÅÌ ÏÐÈ ÍÅÎÄÍÎвÄÍÎÌÓ
ÍÀÏÐÓÆÅÍÎ-ÄÅÔÎÐÌÎÂÀÍÎÌÓ ÑÒÀͲ ÍÀ ÎÑÍβ ÂÈвØÅÍÍß
ÎÁÅÐÍÅÍÈÕ ÇÀÄÀ× ÒÅÐÌÎÏÐÓÆÍÎÑÒ² |
31–34 |
|
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êóõòèí Þ.Ï., |
VERIFICATION of the numerical method For detached flows
SOLUTION |
ÂÅÐÈÔ²ÊÀÖ²ß ÌÅÒÎÄÓ ×ÈÑÅËÜÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß Â²ÄÐÈÂÍÈÕ
ÒÅ×²É ÃÀÇÓ |
ÂÅÐÈÔÈÊÀÖÈß ÌÅÒÎÄÀ
×ÈÑËÅÍÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÎÒÐÛÂÍÛÕ ÒÅ×ÅÍÈÉ ÃÀÇÀ |
35–39 |
Òåðåøèí À.Ì., |
Deceleration of supersonic flow in pseudoshock, hydraulic diameter
concepT |
ÃÀËÜÌÓÂÀÍÍß
ÍÀÄÇÂÓÊÎÂÎÃÎ ÏÎÒÎÊÓ Ó ÏÑÅÂÄÎÑÒÐÈÁÊÓ, ÊÎÍÖÅÏÖ²ß ÃÈÄÐÀÂ˲×ÍÎÃÎ ÄÈÀÌÅÒÐÓ |
ÒÎÐÌÎÆÅÍÈÅ
ÑÂÅÐÕÇÂÓÊÎÂÎÃÎ ÏÎÒÎÊÀ  ÏÑÅÂÄÎÑÊÀ×ÊÅ, ÊÎÍÖÅÏÖÈß ÃÈÄÐÀÂËÈ×ÅÑÊÎÃÎ ÄÈÀÌÅÒÐÀ |
40–45 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ùèïàêîâ Â.À. |
DESIGN AND EXPERIMENTAL ANALYSIS OF THE TURBOCOMPRESSOR UNIT WITH
PULSSATING GAS DYNAMIC RESONATORS |
ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ
ÄÎÑË²ÄÆÅÍÍß ÒÓÐÁÎÊÎÌÏÐÅÑÎÐÍÎÃÎ ÀÃÐÅÃÀÒÓ Ç ÁËÎÊÎÌ ÏÓËÜÑÓÞ×ÈÕ ÃÀÇÎÄÈÍÀ̲×ÍÈÕ
ÐÅÇÎÍÀÒÎв |
46–50 |
|
Áèëåêà Á.Ä., |
ABOUT USING
PROPANE IN THE POWER THERMODYNAMIC CYCLE WITH ISOTHERMAL COMPRESSION OF
WORKING MEDIUM IN POWER UNIT WHICH UTILIZE WASTE HEAT |
ÄÎ ÂÈÊÎÐÈÑÒÀÍÍß ÏÐÎÏÀÍÓ Ó ÑÈËÎÂÎÌÓ
ÒÅÐÌÎÄÈÍÀ̲×ÍÎÌÓ ÖÈÊ˲ Ç ²ÇÎÒÅÐ̲×ÍÈÌ ÑÒÈÑÍÅÍÍßÌ ÐÎÁÎ×ÎÃÎ Ò²ËÀ Â
ÒÅÏËÎÓÒÈ˲ÇÀÖ²ÉÍ²É ÅÍÅÐÃÎÓÑÒÀÍÎÂÖ² |
51–56 |
|
Ìàòâååíêî Â.Ò., |
POWER BOOST GAS
TURBINE ENGINES COMPLETE CYCLES, HEAT RECOVE |
ÔÎÐÑÓÂÀÍÍß ÏÎÒÓÆÍÎÑÒ² ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ
ÄÂÈÃÓÍÀ ÑÊËÀÄÍÎÃÎ ÖÈÊËÓ Ç ÐÅÃÅÍÅÐÀÖ²ªÞ ÒÅÏËÎÒÈ |
ÔÎÐÑÈÐÎÂÀÍÈÅ
ÌÎÙÍÎÑÒÈ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÑËÎÆÍÎÃÎ ÖÈÊËÀ Ñ ÐÅÃÅÍÅÐÀÖÈÅÉ ÒÅÏËÎÒÛ |
57–60 |
Òêà÷ Ì.Ð., |
UTILIZATION OF
LOW POTENTIAL HEAT THE LOW SPEED ICE FROM HYDRIDE TECHNOLOGY |
ÓÒÈ˲ÇÀÖ²ß Í²ÇÊÎÏÎÒÅÍÖ²ÉÍÎÃÎ ÒÅÏËÀ ÌÀËÎÎÁÎÐÎÒÍÈÕ
ÄÂÇ ÍÀ ÁÀDz òÄÐÈÄÍί ÒÅÕÍÎËÎò¯ |
ÓÒÈËÈÇÀÖÈß
ÍÈÇÊÎÏÎÒÅÍÖÈÀËÜÍÎÃÎ ÒÅÏËÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÂÑ ÍÀ ÁÀÇÅ ÃÈÄÐÈÄÍÎÉ ÒÅÕÍÎËÎÃÈÈ |
61–66 |
Ðàä÷åíêî Í.È., |
COOLING
POTENTIAL OF SCAVENGE AIR OF LOW SPEED DIESEL ENGINE OF TRANSPORT SHIP |
ÏÎÒÅÍÖ²ÀË ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ
ÏβÒÐß ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ |
ÏÎÒÅÍÖÈÀË
ÎÕËÀÆÄÅÍÈß ÍÀÄÄÓÂÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ |
67–72 |
Òàðàñåíêî Ì.À., |
extraneous
TEMPERATURE EFFECT ON THE PARAMETERS OF AIR MODES FOR PARTIAL GTE POWER |
âïëèâ
òåìïåðàòóðè çîâí³øíüîãî ïîâ³òðÿ íà ïàðàìåòðè ÷àñòêîâèõ ðåæèì³â ãòä äëÿ
åëåêòðîñòàíö³¿ |
ÂËÈßÍÈÅ
ÒÅÌÏÅÐÀÒÓÐÛ ÍÀÐÓÆÍÎÃÎ ÂÎÇÄÓÕÀ ÍÀ ÏÀÐÀÌÅÒÐÛ ×ÀÑÒÈ×ÍÛÕ ÐÅÆÈÌΠÃÒÄ ÄËß
ÝËÅÊÒÐÎÑÒÀÍÖÈÈ |
73–77 |
Êèñëîâ Î.Â. |
FEATURES OF OPERATION MODE
SELECTION OF CONVERTED GAS TURBINE ENGINE GAS GENERATORS |
ÎÑÎÁËÈÂÎÑÒ² ÂÈÁÎÐÓ ÐÅÆÈÌÓ ÐÎÁÎÒÈ
ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÊÎÍÂÅÐÒÎÂÀÍÎÃÎ ÃÒÄ |
ÎÑÎÁÅÍÍÎÑÒÈ ÂÛÁÎÐÀ
ÐÅÆÈÌÀ ÐÀÁÎÒÛ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÊÎÍÂÅÐÒÈÐÎÂÀÍÍÎÃÎ ÃÒÄ |
78–81 |
Øêàáóðà Â.À. |
ANALYSIS OF
TURBO-COMPRESSOR WITH GENERAL IMPELLER FOR GAS TURBINE ENGINES |
ÄÎÑË²ÄÆÅÍÍß
ÒÓÐÁÎÊÎÌÏÐÅÑÎв ²Ç ÑϲËÜÍÈÌ ÐÎÁÎ×ÈÌ ÊÎËÅÑÎÌ ÄËß ÇÀÑÒÎÑÓÂÀÍÍß Ó ÃÀÇÎÒÓÐÁ²ÍÍÈÕ
ÄÂÈÃÓÍÀÕ |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÒÓÐÁÎÊÎÌÏÐÅÑÑÎÐÎÂ Ñ ÎÁÙÈÌ ÐÀÁÎ×ÈÌ ÊÎËÅÑÎÌ ÏÐÈÌÅÍÈÒÅËÜÍÎ Ê ÃÀÇÎÒÓÐÁÈÍÍÛÌ
ÄÂÈÃÀÒÅËßÌ |
82–85 |
Ëóêàøåâ È.Í., |
EXPERIMENAL
RESEACH OF PROCESS IN THE VAPOR COMPRESSION REFRIGERATION PLANT WITH A
SOLENOID VALVE AS A REGULATOR OF THE REFRIGERANT FLOW |
ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÏÐÎÖÅѲ Ó
ÏÀÐÎÊÎÌÏÐÅÑÎÐÍ²É ÕÎËÎÄÈËÜÍ²É ÌÀØÈͲ Ç ÑÎËÅÍίÄÍÈÌ ÊËÀÏÀÍÎÌ Ó ßÊÎÑÒ²
ÐÅÃÓËßÒÎÐÀ ÂÈÒÐÀÒÈ ÕÎËÎÄÎÀÃÅÍÒÓ |
86–90 |
|
Ðåìèçîâ À.Å., |
to the question of choice of gasodynamic effectiveness parameter
of diffuser |
ÄÎ ÏÈÒÀÍÍß
âÈáîðÓ ïàðàìåòðÓ îö²íêè ãàçîäèíàì²÷Íί Åôåêòèâíîñò² äèôóçîðà |
Ê ÂÎÏÐÎÑÓ ÂÛÁÎÐÀ
ÏÀÐÀÌÅÒÐÀ ÎÖÅÍÊÈ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÄÈÔÔÓÇÎÐÀ |
91–97 |
Êîòêèí Â.Â. |
MATHEMATICAL MODEL OF VISCOUS
INTERACTION OF THE JETS AT THE GAS TURBINE ENGINE NOZZLE EXIT OF MULTI-MODE
AIRCRAFT UNDER SUBSONIC EXTERNAL FLOW |
ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ Â'ßÇÊί ÂÇÀªÌÎIJ¯
ÑÒÐÓÌÅͲ ÍÀ ÂÈÕÎIJ ²Ç ÑÎÏËÀ ÃÒÄ ÁÀÃÀÒÎÐÅÆÈÌÍÎÃΠ˲ÒÀÊÀ  ÓÌÎÂÀÕ ÄÎÇÂÓÊÎÂÎÃÎ
ÇÎÂͲØÍÜÎÃÎ ÎÁÒ²ÊÀÍÍß |
98–102 |
|
Ìàòâååâ Â.Í., |
MULTISTAGE
COMPRESSOR PERFORMANCES IMPROVEMENT BY USING OPTIMIZATION METHODS |
ÏÎË²ÏØÅÍÍß ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÁÀÃÀÒÎÑÒÓϲÍ×ÀÑÒÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÇÀ ÐÀÕÓÍÎÊ ÂÈÊÎÐÈÑÒÀÍÍß ÌÅÒÎIJ ÎÏÒÈ̲ÇÀÖ²¯ |
ÓËÓרÅÍÈÅ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÍÎÃÎÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÇÀ Ñ×¨Ò ÈÑÏÎËÜÇÎÂÀÍÈß ÌÅÒÎÄÎÂ
ÎÏÒÈÌÈÇÀÖÈÈ |
103–107 |
Øåëêîâñêèé Ì.Þ. |
AERODYNAMIC OPTIMIZATION
METHOD OF COMPRESSOR BLADE VANES |
ÌÅÒÎÄ ÀÅÐÎÄÈÍÀ̲×Íί ÎÏÒÈ̲ÇÀÖ²¯
ËÎÏÀÒÊÎÂÈÕ Â²Íֲ ÊÎÌÏÐÅÑÎÐÀ |
ÌÅÒÎÄ
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÎÏÒÈÌÈÇÀÖÈÈ ËÎÏÀÒÎ×ÍÛÕ ÂÅÍÖΠÊÎÌÏÐÅÑÑÎÐÀ |
108–115 |
Ïåòåëü÷èö Â.Þ., |
TO FILM COOLING
RANS SIMULATION ACCURACY IMPROVING APPROACH |
ÄÎ ÏÈÒÀÍÍß Ï²ÄÂÈÙÅÍÍß ÒÎ×ÍÎÑÒ² RANS
ÌÎÄÅËÞÂÀÍÍß Ï˲ÂÊÎÂÎÃÎ ÎÕÎËÎÄÆÅÍÍß |
Ê ÂÎÏÐÎÑÓ
ÏÎÂÛØÅÍÈß ÒÎ×ÍÎÑÒÈ RANS ÌÎÄÅËÈÐÎÂÀÍÈß ÏËÅÍÎ×ÍÎÃÎ ÎÕËÀÆÄÅÍÈß |
116–122 |
Êîðîáêî Â.Â. |
STUDY OF heat transfer and hydrodynamics in Components thermoacoustic
ENGINES |
Äîñë³äæåííÿ
ïðîöåñ³â òåïëîîáì³íó òà ã³äðîäèíàì³êè â åëåìåíòàõ òåðìîàêóñòè÷íèõ äâèãóí³â |
ÈÑÑËÅÄÎÂÀÍÈÅ ÏÐÎÖÅÑÑÎÂ
ÒÅÏËÎÎÁÌÅÍÀ È ÃÈÄÐÎÄÈÍÀÌÈÊÈ Â ÝËÅÌÅÍÒÀÕ ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ ÄÂÈÃÀÒÅËÅÉ |
123–130 |
Ìàðêóøèí À.Í., |
HYDRAULIK CHARACTERISTICS OF SHORTENED MULTI-ATOMIZER COMBUSTOR OF GTE |
òÄÐÀÂ˲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÓÊÎÐÎ×ÅÍί
ÁÀÃÀÒÎÔÎÐÑÓÍÎ×Íί ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÂÌÄ |
ÃÈÄÐÀÂËÈ×ÅÑÊÈÅ
ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÓÊÎÐÎ×ÅÍÍÎÉ ÌÍÎÃÎÔÎÐÑÓÍÎ×ÍÎÉ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß ÃÒÄ |
131–135 |
Êðàâ÷åíêî È.Ô., |
RESEARCH THE IMPACT OF PRESSURE PULSATION IN COMBUSTION CHAMBER ON
STABILITY WORK OF GAS TURBINE ENGINE |
ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÏÀÐÀÌÅÒв ÏÓËÜÑÀÖ²É
ÒÈÑÊÓ Ó ÊÀÌÅв ÇÃÎÐßÍÍß ÍÀ ÑÒ²ÉʲÑÒÜ ÐÎÁÎÒÈ ÃÒÄ |
ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß
ÏÀÐÀÌÅÒÐΠÏÓËÜÑÀÖÈÉ ÄÀÂËÅÍÈß Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÍÀ ÓÑÒÎÉ×ÈÂÎÑÒÜ ÐÀÁÎÒÛ ÃÒÄ |
136–141 |
Êîðíèåíêî Â.Ñ. |
RESEARCH OF SMALL PRODUCTIVITY ROTARY INJECTORS
WORK |
ÄÎÑË²ÄÆÅÍÍß
ÐÎÁÎÒÈ ÐÎÒÀÖ²ÉÍÈÕ ÔÎÐÑÓÍÎÊ ÌÀËί ÏÐÎÄÓÊÒÈÂÍÎÑÒ² |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÐÀÁÎÒÛ ÐÎÒÀÖÈÎÍÍÛÕ ÔÎÐÑÓÍÎÊ ÌÀËÎÉ ÏÐÎÈÇÂÎÄÈÒÅËÜÍÎÑÒÈ |
142–146 |
Ñåðáèí Ñ.È., |
THE NUMERICAL
SIMULATION OF THE PLASMA COAL OXYGEN AND OXYGEN-STEAM GASIFICATION PROCESSES |
×ÈÑÅËÜÍÅ ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ÏËÀÇÌÎÂί
ÊÈÑÍÅÂί ² ÊÈÑÍÅÂÎ-ÏÀÐÎÂί ÃÀÇÈÔÈÊÀÖ²¯ ÂÓòËËß |
×ÈÑËÅÍÍÎÅ
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÖÅÑÑÎÂ ÏËÀÇÌÅÍÍÎÉ ÊÈÑËÎÐÎÄÍÎÉ È ÊÈÑËÎÐÎÄÍÎ-ÏÀÐÎÂÎÉ
ÃÀÇÈÔÈÊÀÖÈÈ ÓÃËÅÉ |
147–150 |
Áîíäàðåíêî Ì.Ñ., |
THE LNG-TERMINAL
REGASIFICATION UNIT WITH GAS-TURBINE FOR ELECTRIC POWER GENERATION |
ÃÒÓ Â ÑÎÑÒÀÂÅ
ÐÅÃÀÇÈÔÈÊÀÖÈÎÍÍÎÃÎ ÊÎÌÏËÅÊÑÀ LNG–ÒÅÐÌÈÍÀËÀ |
151–154 |
|
Ùóêèí Â.À., |
PARTICULARITIES
OF THE FORMATION TOXIC SUBSTANCES IN TURBULENT DIFFUZION COMBUSTION GAS |
ÎÑÎÁËÈÂÎÑÒ² ÓÒÂÎÐÅÍÍß ÒÎÊÑÈ×ÍÈÕ ÐÅ×ÎÂÈÍ
ÏÐÈ ÒÓÐÁÓËÅÍÒÍÎÌÓ ÄÈÔÓDzÉÍÎÌÓ ÇÃÎÐßÍͲ ÃÀDz |
ÎÑÎÁÅÍÍÎÑÒÈ
ÎÁÐÀÇÎÂÀÍÈß ÒÎÊÑÈ×ÍÛÕ ÂÅÙÅÑÒ ÏÐÈ ÒÓÐÁÓËÅÍÒÍÎÌ ÄÈÔÔÓÇÈÎÍÍÎÌ ÃÎÐÅÍÈÈ ÃÀÇΠ|
155–159 |
Íàçèí Â.È. |
THEORY OF DOUBLE RADIAL BEARING IN
GIDROSTATODINAMICHESKOGO STATIONARY EXTERNAL LOAD |
ÒÅÎÐ²ß ÇÄÂΪÍÍß ÐÀIJÀËÜÍÎÃÎ
òÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÏÐÈ ÍÅÑÒÀÖ²ÎÍÀÐÍÎÌÓ ÇÎÂͲØÍÜÎÌÓ ÍÀÂÀÍÒÀÆÅÍͲ |
ÒÅÎÐÈß ÑÄÂÎÅÍÍÎÃÎ
ÐÀÄÈÀËÜÍÎÃÎ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÏÐÈ ÍÅÑÒÀÖÈÎÍÀÐÍÎÉ ÂÍÅØÍÅÉ
ÍÀÃÐÓÇÊÅ |
160–166 |
Äîëìàòîâ Ä.À. |
HYDROXYL AND
ATOMIC OXYGEN GENERATION BY SMALL PLASMA INCLUSIONS |
ÃÅÍÅÐÀÖ²ß Ã²ÄÐÎÊÑÈ˲ ÒÀ ÀÒÎÌÀÐÍÎÃÎ
ÊÈÑÍÞ ÏÎÁËÈÇÓ ÌÀËÈÕ ÏËÀÇÌÎÂÈÕ ÂÊËÞ×ÅÍÜ |
ÃÅÍÅÐÀÖÈß
ÃÈÄÐÎÊÑÈËÎÂ È ÀÒÎÌÀÐÍÎÃÎ ÊÈÑËÎÐÎÄÀ ÂÁËÈÇÈ ÌÀËÛÕ ÏËÀÇÌÅÍÍÛÕ ÂÊËÞ×ÅÍÈÉ |
167–171 |
Âèíîãðàäîâ À.Ñ., |
ANALYSIS OF RADIAL FACE CONTACT SEAL efficiency IN
THE SUPPORT OF THE AIRCRAFT ENGINE COMPRESSOR AT VARIOUS OPERATIONAL MODES |
ÀÍÀ˲Ç
ÏÐÀÖÅÇÄÀÒÍÎÑÒ² ̲ÆÂÀËÜÍÎÃÎ
ÐÀIJÀËÜÍÎ-òîðöåâÎÃÎ ÊÎÍÒÀÊÒÍÎÃÎ ÓÙ²ËÜÍÅÍÍß |
ÀÍÀËÈÇ
ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÈ ÌÅÆÂÀËÜÍÎÃÎ ÐÀÄÈÀËÜÍÎ-ÒÎÐÖÅÂÎÃÎ ÊÎÍÒÀÊÒÍÎÃÎ ÓÏËÎÒÍÅÍÈß |
172–175 |
Òèñàðåâ À.Þ., |
Investigation of labirint sealS perfoRmanCes with
deformations of sealing surfaces |
ÄÎÑË²ÄÆÅÍÍß
ÂÈÒÐÀÒÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ëàá³ðèíòîâîãî óù³ëüíåííÿ Ç ÓÐÀÕÓÂÀÍÍßÌ ÄÅÔÎÐÌÀÖ²É
ÓÙ²ËÜÍÞÂÀËÜÍÈÕ ÏÎÂÅÐÕÎÍÜ |
176–180 |
|
Íîâèêîâ Ä.Ê., |
DEVELOPMENT OF MODEL OF SQUEEZE-FILM
DAMPER WITH METERING GROOVES |
ÐÎÇÐÎÁÊÀ
ÌÎÄÅ˲ òÄÐÎÄÈÍÀ̲×ÍÎÃÎ äåìïôåðà Ç ÄÐÎÑÅËÞÞ×ÈÌÈ êàíàâêàìè |
ÐÀÇÐÀÁÎÒÊÀ ÌÎÄÅËÈ
ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÄÅÌÏÔÅÐÀ Ñ ÄÐÎÑÑÅËÈÐÓÙÈÌÈ ÊÀÍÀÂÊÀÌÈ |
181–184 |
Ñû÷åâà Í.Ñ., |
NEW APPROACH
FOR DESIGNING AND TESTING AN OIL TANK OF A HIGHLY MANUVERING AIR VEHICLE
ENGINE |
ÌÅÒÎÄI×ÍÈÉ ÏIÄÕIÄ ÄÎ ÏÐÎÅÊÒÓÂÀÍÍß ÒÀ ÂÈÏÐÎÁÓÂÀÍÜ
ÌÀÑËßÍÎÃÎ ÁÀÊÀ ÄËß ÄÂÈÃÓÍÀ ÌÀÍÅÂÐÅÍÎÃÎ ËIÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ |
185–188 |
|
Ìîãèëüíèêîâ Â.Ï., |
EQUIPMENT FOR
AIR SAMPLING FROM ENGINE |
ÀÏÀÐÀÒͲ ÇÀÑÎÁÈ ÄËß Â²ÄÁÈÐÀÍÍß ÏÐÎÁ
ÏβÒÐß À²ÀÖ²ÉÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ |
ÀÏÏÀÐÀÒÍÛÅ
ÑÐÅÄÑÒÂÀ ÄËß ÎÒÁÎÐÀ ÏÐÎÁ ÂÎÇÄÓÕÀ ÀÂÈÀÖÈÎÍÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
189–196 |
Îñàä÷èé Í.Â., |
THE ASSURANCE OF CERTIFICATION REQUIREMENTS SHOWN TO THE TURBOFAN
ENGINE FAN CASE |
ÇÀÁÅÇÏÅ×ÅÍÍß
ÑÅÐÒÈÔ²ÊÀÖ²ÉÍÈÕ âèìîã, ùî ïðåä'ÿâëÿþòüñÿ Äî êîðïóñó âåíòèëÿòîðà ÒÐÄÄ |
ÎÁÅÑÏÅ×ÅÍÈÅ ÑÅÐÒÈÔÈÊÀÖÈÎÍÍÛÕ
ÒÐÅÁÎÂÀÍÈÉ, ÏÐÅÄÚßÂËßÅÌÛÕ Ê ÊÎÐÏÓÑÓ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ |
197–200 |
Ïàðîâàé Å.Ô., |
Hydrodynamic bearing with MR elastic suspension
of segments |
òÄÐÎÄÈÍÀ̲×ÍÈÉ Ï²ÄØÈÏÍÈÊ ç ïðóæíèìè ï³äâ³ñîì
âêëàäèø³â ç ÌÀÒÅвÀËÓ ÌÐ |
ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÈÉ
ÏÎÄØÈÏÍÈÊ Ñ ÓÏÐÓÃÈÌ ÏÎÄÂÅÑÎÌ ÂÊËÀÄÛØÅÉ ÈÇ ÌÀÒÅÐÈÀËÀ ÌÐ |
201–205 |
Ëîÿí À.Â., |
ELECTRIC
FIELD HETEROGENEITY MINIMIZATION
DURING TESTS OF EMITTERS IN
ELECTRIC PROPULSION CATHODES |
̲Ͳ̲ÇÀÖ²ß ÍÅÎÄÍÎвÄÍÎÑÒ²
ÅËÅÊÒÐÈ×ÍÎÃÎ ÏÎËß ÏÐÈ ÂÈÏÐÎÁÓÂÀÍÍßÕ Å̲ÒÅв ÊÀÒÎIJ ÅÐÄ |
ÌÈÍÈÌÈÇÀÖÈß
ÍÅÎÄÍÎÐÎÄÍÎÑÒÈ ÝËÅÊÒÐÈ×ÅÑÊÎÃÎ ÏÎËß ÏÐÈ ÈÑÏÛÒÀÍÈßÕ ÝÌÈÒÒÅÐΠÊÀÒÎÄΠÝÐÄ |
206–210 |
Ôåäîð÷åíêî Ä.Ã., |
SPECKLE-INTERFEROMETER
FOR GAS TURBINE ENGINE LARGE-SIZE PARTS AND COMPONENTS VIBRATIONS STUDY |
ÑÏÅÊË-²ÍÒÅÐÔÅÐÎÌÅÒÐ ÄËß ÄÎÑË²ÄÆÅÍÍß
ÊÎËÈÂÀÍÜ ÂÅËÈÊÎÃÀÁÀÐÈÒÍÈÕ ÄÅÒÀËÅÉ ² ÂÓÇ˲ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ |
211–215 |
|
Ðÿáêîâ Â.È., |
HAVE THE HIGGS
BOSON BEEN DISCOVERED |
×È Â²ÄÊÐÈÒÈÉ
ÁÎÇÎÍ Õ²ÃÑÀ? |
216–221 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Êóëèêîâ Ã.Ã., |
MONITORING CONCEPT OF THERMAL STRESS STATE AND BLADE RESOURCE FOR HEAVY-DUTY GAS TURBINES |
ÊÎÍÖÅÏÖ²ß
ÌÎͲÒÎÐÈÍÃÓ ÒÅÐÌÎÍÀÏÐÓÆÅÍÎÃÎ ÑÒÀÍÓ ² ÐÅÑÓÐÑÓ ËÎÏÀÒÎÊ ÂÈÑÎÊÎÍÀÂÀÍÒÀÆÅÍÈÕ
ÒÓÐÁ²Í À²ÀÖ²ÉÍÈÕ ÃÒÄ |
222–228 |
|
Goncharenko A.V. |
ÏÐÈÍÖÈÏ
ÅÊÑÒÐÅ̲ÇÀÖ²¯ ÑÓÁ’ªÊÒÈÂÍί ÅÍÒÐÎϲ¯ ßÊ ²ÍÑÒÐÓÌÅÍÒ ÊÅÐÓÂÀÍÍß ÌÀÊÑÈÌÀËÜÍÎÞ ÒÐÈÂÀ˲ÑÒÞ
ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÜÎÒÓ Ë²ÒÀÊÀ |
ÏÐÈÍÖÈÏ ÝÊÑÒÐÅÌÈÇÀÖÈÈ ÑÓÁÚÅÊÒÈÂÍÎÉ
ÝÍÒÐÎÏÈÈ ÊÀÊ ÈÍÑÒÐÓÌÅÍÒ ÓÏÐÀÂËÅÍÈß ÌÀÊÑÈÌÀËÜÍÎÉ ÏÐÎÄÎËÆÈÒÅËÜÍÎÑÒÜÞ
ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÅÒÀ ÑÀÌÎËÅÒÀ |
229–234 |
|
Ïàí³í Â.Â., |
COMBINED MODELS
OF INFORMATION PROCESSING IN THE ELECTRONIC CONTROL SYSTEMS OF AIRCRAFT
ENGINES |
ÊÎÌÁ²ÍÎÂÀͲ ÌÎÄÅ˲
ÎÁÐÎÁÊÈ ²ÍÔÎÐÌÀÖ²¯  ÅËÅÊÒÐÎÍÍÈÕ ÑÈÑÒÅÌÀÕ ÊÅÐÓÂÀÍÍß À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÊÎÌÁÈÍÈÐÎÂÀÍÍÛÅ
ÌÎÄÅËÈ ÎÁÐÀÁÎÒÊÈ ÈÍÔÎÐÌÀÖÈÈ Â ÝËÅÊÒÐÎÍÍÛÕ ÑÈÑÒÅÌÀÕ ÓÏÐÀÂËÅÍÈß ÀÂÈÀÖÈÎÍÍÛÕ
ÄÂÈÃÀÒÅËÅÉ |
235–239 |
Áóðÿ÷åíêî À.Ã., |
PARAMETRIC RELIABILITY RESEARCH RESULTS OF AIRCRAFT PRESSURE
TRANSDUCERS |
ÐÅÇÓËÜÒÀÒÈ ÄÎÑËIÄÆÅÍÍß
ÏÀÐÀÌÅÒÐÈ×Íί ÍÀÄIÉÍÎÑÒ² ÀÂÈÀÖIÉÍÈÕ ÄÀÒ×ÈÊI ÒÈÑÊÓ |
ÐÅÇÓËÜÒÀÒÛ
ÈÑÑËÅÄÎÂÀÍÈß ÏÀÐÀÌÅÒÐÈ×ÅÑÊÎÉ ÍÀÄÅÆÍÎÑÒÈ ÀÂÈÀÖÈÎÍÍÛÕ ÄÀÒ×ÈÊΠÄÀÂËÅÍÈß |
240–245 |
Ìèðãîðîä Â.Ô., |
CLUSTERS EXTRACTION AT MULTIDIMENSIONAL TREND ANALYSIS |
ÂÈIJËÅÍÍß ÊËÀÑÒÅвÂ
ÏÐÈ ÁÀÃÀÒÎÂÈ̲ÐÍÎÌÓ ÒÐÅÍÄÎÂÎÌ ÀÍÀ˲Dz |
246–249 |
|
Äàâèäåíêî Â.Î. |
METHOD OF COMPUTER MONITORING OF THE
ZONE OF CHEMICAL POLLUTION IN CASE OF EMERGENCY EMISSIONS OF POISONING
CHEMICALS IN THE ATMOSPHERE |
ÌÅÒÎÄ ÊÎÌÏ'ÞÒÅÐÍÎÃÎ ÌÎͲÒÎÐÈÍÃÓ ÇÎÍÈ
ղ̲×ÍÎÃÎ ÇÀÁÐÓÄÍÅÍÍß ÏÐÈ ÀÂÀвÉÍÈÕ ÂÈÊÈÄÀÕ ÎÒÐÓÉËÈÂÈÕ Õ²Ì²×ÍÈÕ ÐÅ×ÎÂÈÍ Â
ÀÒÌÎÑÔÅÐÓ |
250–254 |
|
Òðåòüÿê Â.Â., |
DEVELOPMENT OF INFORMATION AND
MATHEMATICAL MODEL FOR CALCULATING THE ECONOMIC EFFICIENCY CAD PULSED
PROCESSES |
ÐÎÇÐÎÁÊÀ ÌÀÒÅÌÀÒÈ×Íί ÒÀ ²ÍÔÎÐÌÀÖ²ÉÍί
ÌÎÄÅ˲ ÄËß ÐÎÇÐÀÕÓÍÊÓ ÅÊÎÍÎ̲×Íί ÅÔÅÊÒÈÂÍÎÑÒ² ÂÈÊÎÐÈÑÒÀÍÍß ÑÀÏÐ ²ÌÏÓËÜÑÍÈÕ
ÏÐÎÖÅѲ |
255–259 |
|
Êó÷óê Ã.À. |
MODELLING OF THE WIRELESS NETWORK AGGREGATED TRAFFIC ON THE BASIS OF
INFORMATIVE STREAMS STATISTICAL MONITORING |
ÌÎÄÅËÞÂÀÍÍß ÀÃÐÅÃÎÂÀÍÎÃÎ ÒÐÀÔ²ÊÀ ÁÅÇÏÐβÄÍί ÌÅÐÅÆ² ÏÅÐÅÄÀײ ÄÀÍÈÕ, ÙÎ
¥ÐÓÍÒÓªÒÜÑß ÍÀ ÑÒÀÒÈÑÒÈ×ÍÎÌÓ ÌÎͲÒÎÐÈÍDz ²ÍÔÎÐÌÀÖ²ÉÍÈÕ ÏÎÒÎʲ |
260–264 |
|
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè |
||||
Íåñòåðåíêî Â.Ã., |
COMPREHENSIVE TRAINING
OF UNIVERSITY STUDENTS IN «AIRCRAFT ENGINES AND POWER PLANTS» |
ÊÎÌÏËÅÊÑÍÀ ϲÄÃÎÒÎÂÊÀ Ó×Ͳ ÂÈÙÈÕ
ÍÀÂ×ÀËÜÍÈÕ ÇÀÊËÀIJ ÇÀ ÑÏÅÖ²ÀËÜͲÑÒÞ
«À²ÀÖ²ÉͲ ÄÂÈÃÓÍÈ ² ÅÍÅÐÃÅÒÈ×Ͳ ÓÑÒÀÍÎÂÊÈ» |
265–268 |
|
Ñòåïàíåíêî Ñ.Ì., |
ESTIMATION OF QUALITY MANAGEMENT SYSTEMS PROCESSS EFFECTIVENESS
OF COMPANIES INVOLVED IN DESIGN OF AVIATION PRODUCTS |
ÎÖ²ÍÊÀ ÐÅÇÓËÜÒÀÒÈÂÍÎÑÒ² ÏÐÎÖÅѲ ÑÈÑÒÅÌ ÌÅÍÅÄÆÌÅÍÒÓ
ßÊÎÑÒ² ϲÄÏÐȪÌÑÒ ÐÎÇÐÎÁÍÈʲÂ
À²ÀÖ²ÉÍί ÒÅÕͲÊÈ |
269–272 |
|
Ðåâà Î.Ì., |
LEVEL OF CLAIMS
OF AIR TRAFFIC CONTROLLERS FOR RESULTS OF WORKING LOAD |
вÂÅÍÜ ÄÎÌÀÃÀÍÜ
À²ÀÄÈÑÏÅÒ×Åв ÍÀ ÏÎÊÀÇÍÈÊÀÕ ÐÎÁÎ×ÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß |
ÓÐÎÂÅÍÜ ÏÐÈÒßÇÀÍÈÉ
ÀÂÈÀÄÈÑÏÅÒ×ÅÐΠÍÀ ÏÎÊÀÇÀÒÅËßÕ ÐÀÁÎ×ÅÉ ÍÀÃÐÓÇÊÈ |
273–281 |
Äàíîâà Ì.À. |
SYNTHESIS MODEL SELECTION OF
PRIORITIES FOR PREDICTING THE SCIENTIFIC AND TECHNICAL DEVELOPMENT USING
TECHNOLOGY FORESIGHT |
ÑÈÍÒÅÇ ÌÎÄÅ˲ ÂÈÁÎÐÓ ÏвÎÐÈÒÅҲ ÏÐÈ ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÈ
ÍÀÓÊÎÂÎ-ÒÅÕͲ×ÍÎÃÎ ÐÎÇÂÈÒÊÓ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÒÅÕÍÎËÎò¯ ÔÎÐÑÀÉÒ |
282–286 |
|
Äåìüÿíåíêî Â.À. |
INFORMATION
SUPPORT OF PRODUCTION OF CONSUMER GOODS AT MULTIPRODUCT MACHINE-BUILDING
ENTERPRISE |
²ÍÔÎÐÌÀÖ²ÉÍÀ ϲÄÒÐÈÌÊÀ ÂÈÐÎÁÍÈÖÒÂÀ
ÒÎÂÀв ÍÀÐÎÄÍÎÃÎ ÑÏÎÆÈÂÀÍÍß ÍÀ ÁÀÃÀÒÎÍÎÌÅÍÊËÀÒÓÐÍÎÌÓ ÌÀØÈÍÎÁÓIJÂÍÎÌÓ
ϲÄÏÐȪÌÑÒ² |
287–292 |
Óâàæàåìûå ÷èòàòåëè!
Íàó÷íî-òåõíè÷åñêèé
æóðíàë «Àâèàöèîííî-êîñìè÷åñêàÿ òåõíèêà è òåõíîëîãèÿ»
- âõîäèò â óòâåðæäåííûé ÃÀÊ Ïåðå÷åíü íàó÷íûõ
ïðîôåññèîíàëüíûõ èçäàíèé Óêðàèíû, â êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ ðåçóëüòàòû
äèññåðòàöèîííûõ ðàáîò íà ñîèñêàíèå ó÷åíûõ ñòåïåíåé äîêòîðà è êàíäèäàòà íàóê (ñì. ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû
¹1-05/4 îò 14.10.2009 ã.);
– ñîõðàíÿåòñÿ â
îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà íàóêîâà» è ïóáëèêóåòñÿ
â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ óêðàèíñêîãî ðåôåðàòèâíîãî æóðíàëà «Äæåðåëî»
(ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua) (Óêðàèíà),
– ñîõðàíÿåòñÿ â ðåôåðàòèâíîé áàçå äàííûõ Âñåðîññèéñêîãî
èíñòèòóòà íàó÷íîé è òåõíè÷åñêîé èíôîðìàöèè (ÂÈÍÈÒÈ) Ðîññèéñêîé àêàäåìèè íàóê è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ
òåìàòè÷åñêèõ ñåðèÿõ ÐÆ (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.viniti.ru) (Ðîññèéñêàÿ
Ôåäåðàöèÿ),
- âêëþ÷åí â ìåæäóíàðîäíûå
íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU
(Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.