Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 8
(125). – 143 ñ.
ISSN 1727-7337.
ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 8 (125). – 143 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 8 (125). – 143 ñ.
Ìàòåðèàëû,
ñîäåðæàùèåñÿ â æóðíàëå, îïóáëèêîâàíû
ïî ðåøåíèþ XX ìåæäóíàðîäíîãî êîíãðåññà äâèãàòåëåñòðîèòåëåé
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè (article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
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Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
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Ìîçãîâîé Â. Ô., |
MODERN METHODES
OF PRELIMINERY PROCESSING MONOWHEELS OF TURBINE ENGINS ON MACHIN CNC |
ÑÓ×ÀÑͲ ÌÅÒÎÄÈ
ÏÎÏÅÐÅÄÍÜί ÎÁÐÎÁÊÈ ÌÎÍÎÊÎËÅÑ ÃÒÄ ÍÀ ÂÅÐÑÒÀÒÀÕ Ç ×ÏÊ |
ÑÎÂÐÅÌÅÍÍÛÅ ÌÅÒÎÄÛ
ÏÐÅÄÂÀÐÈÒÅËÜÍÎÉ ÎÁÐÀÁÎÒÊÈ ÌÎÍÎÊÎ謄 ÃÒÄ ÍÀ ÑÒÀÍÊÀÕ Ñ ×ÏÓ |
5–10 |
Ïåòðèê È. À., |
DEVELOPING POWDERS OF TITANIUM ALLOYS FOR
ADDITIVE TECHNOLOGIES AS APPLIED TO GAS TURBINE ENGINE PARTS |
ÐÎÇÐÎÁÊÀ ÏÎÐÎØÊ²Â ÒÈÒÀÍÎÂÈÕ
ÑÏËÀ² ÄËß ÀÄÈÒÈÂÍÈÕ ÒÅÕÍÎËÎÃ²É ÑÒÎÑÎÂÍÎ ÄÎ ÄÅÒÀËÅÉ ÃÒÄ |
ÐÀÇÐÀÁÎÒÊÀ ÏÎÐÎØÊÎÂ
ÒÈÒÀÍÎÂÛÕ ÑÏËÀÂΠÄËß ÀÄÄÈÒÈÂÍÛÕ ÒÅÕÍÎËÎÃÈÉ ÏÐÈÌÅÍÈÒÅËÜÍÎ Ê ÄÅÒÀËßÌ ÃÒÄ |
11–16 |
Ñèíÿºâà Í. Ï. |
DETERMINATION OF ALLOYING ELEMENTS IN THE SUPERALLOYS ON THE BASIS OF NICKEL BY ATOMIC-ABSORPTION METHOD |
ÂÈÇÍÀ×ÅÍÍß ËÅÃÓÞ×ÈÕ
ÅËÅÌÅÍÒ²Â Ó ÆÀÐÎ̲ÖÍÈÕ ÑÏËÀÂÀÕ ÍÀ ÎÑÍβ ͲÊÅËÞ ÀÒÎÌÍÎ-ÀÁÑÎÐÁÖ²ÉÍÈÌ ÌÅÒÎÄÎÌ |
ÎÏÐÅÄÅËÅÍÈÅ ËÅÃÈÐÓÞÙÈÕ
ÝËÅÌÅÍÒΠ ÆÀÐÎÏÐÎ×ÍÛÕ ÑÏËÀÂÀÕ ÍÀ ÎÑÍΊͲÊÅËß ÀÒÎÌÍÎ-ÀÁÑÎÐÁÖÈÎÍÍÛÌ
ÌÅÒÎÄÎÌ |
17–21 |
Ñíåæíîé Ã. Â., |
INFLUENCE OF CHEMICAL COMPONENTS ON MECHANICAL
AND MAGNETIC PROPERTIES MANGANESE STEELS |
ÂÏËÈ ղ̲×ÍÈÕ ÊÎÌÏÎÍÅÍҲ ÍÀ ÌÅÕÀͲ×Ͳ
² ÌÀÃͲÒͲ ÂËÀÑÒÈÂÎÑÒ² ÂÈÑÎÊÎÌÀÐÃÀÍÖÅÂÈÕ ÑÒÀËÅÉ |
ÂËÈßÍÈÅ ÕÈÌÈ×ÅÑÊÈÕ ÊÎÌÏÎÍÅÍÒΠÍÀ ÌÅÕÀÍÈ×ÅÑÊÈÅ
È ÌÀÃÍÈÒÍÛÅ ÑÂÎÉÑÒÂÀ ÂÛÑÎÊÎÌÀÐÃÀÍÖÅÂÛÕ ÑÒÀËÅÉ |
22–26 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Forghany
F., |
NUMERICAL STUDY OF
THE AERODYNAMIC EFFECTS ON FLUIDIC THRUST VECTORING |
×ÈÑÅËÜÍÅ ÄÎÑË²ÄÆÅÍÍß
ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÌÅÒÎIJ ÊÅÐÓÂÍÍß ÂÅÊÒÎÐÎÌ ÒßÃÈ |
×ÈÑËÅÍÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÌÅÒÎÄΠÓÏÐÀÂËÅÍÈß ÂÅÊÒÎÐÎÌ ÒßÃÈ |
27–34 |
Ïðèõîäüêî À. À., |
ICING
OF AIRFOILS: METHODOLOGY OF ICE ACCRETION |
ÎÁÌÅÐÇÀÍÍß ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÏÎÂÅÐÕÎÍÜ: ÌÅÒÎÄÈÊÀ
ÌÎÄÅËÞÂÀÍÍß ÍÀÐÎÑÒÀÍÍß ÊÐÈÃÈ |
ÎÁËÅÄÅÍÅÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ
ÏÎÂÅÐÕÍÎÑÒÅÉ: ÌÅÒÎÄÈÊÀ ÌÎÄÅËÈÐÎÂÀÍÈß ÍÀÐÀÑÒÀÍÈß ËÜÄÀ |
35–45 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
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Ðóñàíîâ À. Â., |
MODELING OF VISCOUS
FLOWS IN FLOW PARTS OF POWER TURBINES USING THE DIFFERENT EQUATIONS OF STATE |
ÌÎÄÅËÞÂÀÍÍß ÏÐÎÑÒÎÐÎÂÈÕ Â'ßÇÊÈÕ ÒÅײ¯ Ó
ÏÐÎÒÎ×ÍÈÕ ×ÀÑÒÈÍÀÕ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÒÓÐÁ²Í ²Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ Ð²ÇÍÈÕ Ð²ÂÍßÍÜ ÑÒÀÍÓ |
46–51 |
|
Êîðîáêî Â. Â. |
ANALYSIS OF OPPORTUNITIES FOR IMPROVEMENTS
OF THERMOACOUSTIC HEAT ENGINES THROUGH THE HEAT EXCHANGE PROCESSES RATIONALIZATION |
ÀÍÀËÈÇ ÂÎÇÌÎÆÍÎÑÒÅÉ
ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈß ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ ÒÅÏËÎÂÛÕ ÌÀØÈÍ ÏÓÒÅÌ ÐÀÖÈÎÍÀËÜÍÎÉ ÎÐÃÀÍÈÇÀÖÈÈ
ÏÐÎÖÅÑÑÀ ÒÅÏËÎÎÁÌÅÍÀ |
52–57 |
|
Æóëàé Þ. À. |
THEORETICAL EVALUTATION OF EFFICIENCY FACTOR
OF VORTEX HEAT GENERATOR |
ÒÅÎÐÅÒÈ×ÍÀ ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² ÊÀ²ÒÀÖ²ÉÍÎÃÎ
ÒÅÏËÎÃÅÍÅÐÀÒÎÐÀ |
ÒÅÎÐÅÒÈ×ÅÑÊÀß ÎÖÅÍÊÀ
ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÀÂÈÒÀÖÈÎÍÍÎÃÎ ÒÅÏËÎÃÅÍÅÐÀÒÎÐÀ |
58–64 |
Ëîÿí À. Â., |
RESULTS OF MIRCRO
MASS FLOW CATHODE-NEUTRALIZER WITH OPERATING CURRENT UP TO 300 MA DEVELOPMENT
AND TESTING |
ÐÅÇÓËÜÒÀÒÈ ÐÎÇÐÎÁÊÈ É ÂÈÏÐÎÁÓÂÀÍÜ Ì²ÊÐÎ
ÂÈÒÐÀÒÍÎÃÎ ÊÀÒÎÄÓ-ÍÅÉÒÐÀ˲ÇÀÒÎÐÓ ÍÀ ÐÎÁÎײ ÑÒÐÓÌÈ ÄÎ 300 ÌÀ |
ÐÅÇÓËÜÒÀÒÛ ÐÀÇÐÀÁÎÒÊÈ
È ÈÑÏÛÒÀÍÈÉ ÌÈÊÐÎ ÐÀÑÕÎÄÍÎÃÎ ÊÀÒÎÄÀ-ÍÅÉÒÐÀËÈÇÀÒÎÐÀ ÍÀ ÐÀÁÎ×ÈÅ ÒÎÊÈ ÄÎ 300 ÌÀ |
65–69 |
Ñîðîãèí Ô. Ã., |
EXPERIMENTAL
INVESTIGATION OF THE GAS TURBINE UNIT CYCLIC AIR SPRAY COOLING SYSTEM |
ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑËIÄÆÅÍÍß ÐÎÇÏÈËÞÂÀËÜÍί
ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÃÒÏ |
ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ
ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÑÏÛËÈÒÅËÜÍÎÉ ÑÈÑÒÅÌÛ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÃÒÏ |
70–74 |
Òèìîøåíêî Â. È., |
ON THE RATIONAL IMPLEMENTATION OF PROCESSES
OF MIXING AND COMBUSTION WITHIN RAMJET COMBUSTION CHAMBER |
ÄÎ ÏÈÒÀÍÍß ÐÀÖ²ÎÍÀËÜÍί ÎÐÃÀͲÇÀÖ²¯ ÏÐÎÖÅѲÂ
Ç̲ØÓÂÀÍÍß ² ÃÎвÍÍß Â ÊÀÌÅв ÇÃÎÐßÍÍß ÏÏÐÄ |
Ê ÂÎÏÐÎÑÓ Î ÐÀÖÈÎÍÀËÜÍÎÉ
ÎÐÃÀÍÈÇÀÖÈÈ ÏÐÎÖÅÑÑÎÂ ÑÌÅØÅÍÈß È ÃÎÐÅÍÈß Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÏÂÐÄ |
75–81 |
Òèòîâ Ì. Þ., |
MEASUREMENTS OF PROBE CHARACTERISTICS IN THE DISCHARGE CHANNEL OF STATIONARY PLASMA THRUSTER |
ÂÈ̲ÐÞÂÀÍÍß ÇÎÍÄÎÂÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ó
ÐÎÇÐßÄÍÎÌÓ ÊÀÍÀ˲ ÑÒÀÖ²ÎÍÀÐÍÎÃÎ
ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ |
ÈÇÌÅÐÅÍÈÅ ÇÎÍÄÎÂÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
 ÐÀÇÐßÄÍÎÌ ÊÀÍÀËÅ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÄÂÈÃÀÒÅËß |
82–88 |
Òêà÷ Ì. Ð., |
RESEARCH STAND BASED
ON PARAMETERS OF TORSIONAL VIBRATIONS ON LOW SPEED DIESEL ENGINE FOR DETERMINATION
OF SIZE EFFECT |
ÑÒÅÍÄ ÄËß ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÌÀÑØÒÀÁÍÎÃÎ
ÔÀÊÒÎÐÓ ÍÀ ÏÀÐÀÌÅÒÐÈ ÊÐÓÒÈËÜÍÈÕ ÊÎËÈÂÀÍÜ ÅÍÅÐÃÅÒÈ×ÍÈÕ ÓÑÒÀÍÎÂÎÊ Ç ÌÎÄ |
89–92 |
|
Åïèôàíîâ Ñ. Â., |
TURBOFAN TECHNICAL
CONDITION FORECAST |
ÏÐÎÃÍÎÇÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ
ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ |
ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÒÅÕÍÈ×ÅÑÊÎÃÎ
ÑÎÑÒÎßÍÈß ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß |
93–101 |
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Ãâîçäåâà È. Ì. |
THE DIRECTIONAL CHARACTERISTICS OPTIMIZATION OF ACOUSTIC SENSORS SYSTEMS |
ÎÏÒÈ̲ÇÀÖ²ß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÏÐßÌÎÂÀÍÎÑÒ² ÑÈÑÒÅÌ ÀÊÓÑÒÈ×ÍÈÕ ÄÀÒ×Èʲ |
ÎÏÒÈÌÈÇÀÖÈß ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÍÀÏÐÀÂËÅÍÍÎÑÒÈ ÑÈÑÒÅÌ ÀÊÓÑÒÈ×ÅÑÊÈÕ ÄÀÒ×ÈÊΠ|
102–106 |
Ãîæèé Î. Ï., |
DISTRIBUTION OF ENERGY RESOURCES MODELING
BASED ON COLOR PETRI NETS |
ÌÎÄÅËÞÂÀÍÍß ÐÎÇÏÎIJËÓ
ÅÍÅÐÃÅÒÈ×ÍÈÕ ÐÅÑÓÐѲ ÍÀ ÎÑÍβ ÊÎËÜÎÐÎÂÈÕ ÌÅÐÅÆ ÏÅÒв |
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÐÀÑÏÐÅÄÅËÅÍÈß ÅÍÅÐÃÅÒÈ×ÅÑÊÈÕ
ÐÅÑÓÐÑÎÂ ÍÀ ÎÑÍÎÂÅ ÖÂÅÒÍÛÕ ÑÅÒÅÉ ÏÅÒÐÈ |
107–111 |
Æóðàâë¸â Â. Í. |
PHENOMENOLOGICAL MODEL OF PROCESS OF RADIATION OF ENERGY OF THE SOUND IN
THE COURSE OF DETONATION COMBUSTION |
ÔÅÍÎÌÅÍÎËÎò×ÍÀ
ÌÎÄÅËÜ ÏÐÎÖÅÑÓ ÂÈÏÐÎ̲ÍÞÂÀÍÍß ÅÍÅÐò¯ ÇÂÓÊÓ Â ÏÐÎÖÅѲ ÃÎвÍÍß |
ÔÅÍÎÌÅÍÎËÎÃÈ×ÅÑÊÀß
ÌÎÄÅËÜ ÏÐÎÖÅÑÑÀ ÈÇËÓ×ÅÍÈß ÝÍÅÐÃÈÈ ÇÂÓÊÀ  ÏÐÎÖÅÑÑÅ ÃÎÐÅÍÈß |
112–118 |
²ãíàòê³í Â. Ó., |
CORRECTION FOR CALIBRATION INTERVAL OF MEASURING
EQUIPMENT AT THEIR CURRENT TECHNICAL STATES |
ÊÎÐÐÅÊÒÈÐÎÂÊÀ ÄËÈÒÅËÜÍÎÑÒÈ ÌÅÆÏÎÂÅÐÎ×ÍÛÕ
ÈÍÒÅÐÂÀËΠÑÐÅÄÑÒ ÈÇÌÅÐÈÒÅËÜÍÎÉ ÒÅÕÍÈÊÈ ÏÎ ÈÕ ÒÅÊÓÙÅÌÓ ÒÅÕÍÈ×ÅÑÊÎÌÓ ÑÎÑÒÎßÍÈÞ |
119–122 |
|
Ðåâà Î. Ì., |
INTEGRATIVE MODEL OF ASSESSMENT AIR TRAFFIC
CONTROLLERS TO VIOLATION OF THE SPERATION IN THE AIRSPACE |
ÌÎÄÅËÜ ÈÍÒÅÃÐÀÒÈÂÍÎÉ ÎÖÅÍÊÈ ÎÒÍÎØÅÍÈß ÀÂÈÀÄÈÑÏÅÒ×ÅÐÎÂ
Ê ÍÀÐÓØÅÍÈßÌ ÍÎÐÌÛ ÝØÅËÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ |
123–129 |
|
Ñåì÷èøèí Ñ. Ì., |
PORTABLE AUTOMATED
PARAMETERS RECORDER– EXTENTION OF FUNCTIONAL CAPABILITIES |
ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÉ ÐŪÑÒÐÀÒÎÐ ÏÀÐÀÌÅÒв ÏÅÐÅÍÎÑÍÈÉ
– ÐÎÇØÈÐÅÍÍß ÔÓÍÊÖ²ÎÍÀËÜÍÈÕ ÌÎÆËÈÂÎÑÒÅÉ |
ÀÂÒÎÌÀÒÈÇÈÐÎÂÀÍÍÛÉ
ÐÅÃÈÑÒÐÀÒÎÐ ÏÀÐÀÌÅÒÐÎÂ ÏÅÐÅÍÎÑÍÎÉ – ÐÀÑØÈÐÅÍÈÅ ÔÓÍÊÖÈÎÍÀËÜÍÛÕ ÂÎÇÌÎÆÍÎÑÒÅÉ |
130–133 |
Òðåòüÿê Â. Â. |
THE IMPLEMENTATION
OF THE CLASSIFICATION PHASE IN THE SYSTEM SPRUT TO DEVELOP NEW PROCESSES OF PULSE
TECHNOLOGIES |
ÐÅÀ˲ÇÀÖ²ß ÊËÀÑÈÔ²ÊÀÖ²ÉÍÎÃÎ ÅÒÀÏÓ Â ÑÈÑÒÅ̲
ÑÏÐÓÒ ÄËß ÐÎÇÐÎÁÊÈ ÍÎÂÈÕ ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍÈÕ ÒÅÕÍÎËÎÃ²É |
134–137 |
|
Èâàùåíêî À. È., |
AUTOMATION OF
TECHNOLOGICAL PROCESS CHECKS ELECTRICAL HARNESSES GTE OF THE AIRCRAFT |
ÀÂÒÎÌÀÒÈÇÀÖ²ß ÒÅÕÍÎËÎò×ÍÎÃÎ ÏÐÎÖÅÑÓ ÏÅÐŲÐÊÈ
ÅËÅÊÒÐÈ×ÍÈÕ ÄÆÃÓҲ À²ÀÖ²ÉÍÈÕ ÃÒÄ |
ÀÂÒÎÌÀÒÈÇÀÖÈß
ÒÅÕÍÎËÎÃÈ×ÅÑÊÎÃÎ ÏÐÎÖÅÑÑÀ ÏÐÎÂÅÐÊÈ ÝËÅÊÒÐÈ×ÅÑÊÈÕ ÆÃÓÒΠÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ |
138–141 |
142 |
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 (ïðèêàç ÌÎÍ Óêðàèíû ¹1279 îò 6.11.2014 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
áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé
áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ);
Index Copernicus (ICV 2013: 4,83) (Ïîëüøà); Google Scholar (áèáëèîìåòðè÷åñêèå
ïîêàçàòåëè – quot.=2094 / h = 10 / i10 = 15).