ÍÀÖ²ÎÍÀËÜÍÈÉ ÀÅÐÎÊÎÑ̲×ÍÈÉ ÓͲÂÅÐÑÈÒÅÒ ²Ì. Ì. ª. ÆÓÊÎÂÑÜÊÎÃÎ "ÕÀÐʲÂÑÜÊÈÉ À²ÀÖ²ÉÍÈÉ ²ÍÑÒÈÒÓÒ"

 

ISSN: 1727-7337 (Print)2663-2217 (Online). À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2020. – ¹ 7(167). – 160 ñ.

ISSN: 1727-7337 (Print)2663-2217 (Online). ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2020. – ¹ 7(167). – 160 ñ.

ISSN: 1727-7337 (Print)2663-2217 (Online). AEROSPACE TECHNIC AND TECHNOLOGY. – 2020. – No. 7(167). – 160 p.

 

 

Òåìàòè÷íèé âèïóñê «Ïðîáëåìè äâèãóíîáóäóâàííÿ»

 

 

ÑÒÀÒÒ² (articleS)

 

Àâòîðè
(
ìîâà îðèã³íàëó)

Íàçâà ñòàòò³ (article title)

Ñòîð³íêè

(pages)

English

Óêðà¿íñüêà ìîâà

Ðîñ³éñüêà ìîâà

Ïðîåêòóâàííÿ ë³òàëüíèõ àïàðàò³â

Ëîñü À. Â.,
Ðÿáêîâ Â. È.,
Ñåðåäà Ò. Í. 

PROBLEMS OF CREATION OF AIRCRAFT CATEGORY PLANES ACCORDING TO ENVIRONMENTAL LIMITATIONS

ÏÐÎÁËÅÌÈ ÑÒÂÎÐÅÍÍß Ë²ÒÀʲ ÒÐÀÍÑÏÎÐÒÍί ÊÀÒÅÃÎв¯ Ç ÓÐÀÕÓÂÀÍÍßÌ ÅÊÎËÎò×ÍÈÕ ÎÁÌÅÆÅÍÜ

ÏÐÎÁËÅÌÛ ÑÎÇÄÀÍÈß ÑÀÌÎËÅÒΠÒÐÀÍÑÏÎÐÒÍÎÉ ÊÀÒÅÃÎÐÈÈ Ñ Ó×ÅÒÎÌ ÝÊÎËÎÃÈ×ÅÑÊÈÕ ÎÃÐÀÍÈ×ÅÍÈÉ

5–11

Òåîð³ÿ ³ ðîáî÷³ ïðîöåñè àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê

Òêà÷ Ì. Ð.,
Ïðîñêóð³í À. Þ.,
Ìèòðîôàíîâ Î. Ñ.,
Ãàëèíê³í Þ. Ì.

INCREASING THE EFFICIENCY OF HYDROGEN PRODUCTION TECHNOLOGY BY USING A REGENERATION CIRCUIT WITH A ROTARY-PISTON EXPANDER MACHINE

ϲÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÒÅÕÍÎËÎò¯ ÎÒÐÈÌÀÍÍß ÂÎÄÍÞ ØËßÕÎÌ ÂÈÊÎÐÈÑÒÀÍÍß ÐÅÃÅÍÅÐÀÖ²ÉÍÎÃÎ ÊÎÍÒÓÐÓ Ç ÐÎÒÎÐÍÎ-ÏÎÐØÍÅÂÎÞ ÐÎÇØÈÐÞÂÀËÜÍÎÞ ÌÀØÈÍÎÞ

ÏÎÂÛØÅÍÈÅ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÒÅÕÍÎËÎÃÈÈ ÏÎËÓ×ÅÍÈß ÂÎÄÎÐÎÄÀ ÏÓÒÅÌ ÈÑÏÎËÜÇÎÂÀÍÈß ÐÅÃÅÍÅÐÀÖÈÎÍÍÎÃÎ ÊÎÍÒÓÐÀ Ñ ÐÎÒÎÐÍÎ-ÏÎÐØÍÅÂÎÉ ÐÀÑØÈÐÈÒÅËÜÍÎÉ ÌÀØÈÍÎÉ

12–18

Óñåíêî Â. Þ.,
Äîðîøåíêî Ê. Â.,
Õèæíÿê Ì. Â.

EFFECT OF THE CLEARANCE BETWEEN ROWS OF COAXIAL PROPFAN ON THRUST

ÂÏËÈ ÇÀÇÎÐÓ Ì²Æ ÐßÄÀÌÈ Ñϲ²ÑÍÎÃÎ ÏβÒÐßÍÎÃÎ ÃÂÈÍÒÀ ÍÀ ÒßÃÓ

ÂËÈßÍÈÅ ÇÀÇÎÐÀ ÌÅÆÄÓ ÐßÄÀÌÈ ÑÎÎÑÍÎÃÎ ÂÎÇÄÓØÍÎÃÎ ÂÈÍÒÀ ÍÀ ÒßÃÓ

19–23

Ðîìàíåíêî È. Ñ.,
Áåëîãóá À. Â.

FUEL GEAR PUMP OF GAS TURBINE ENGINE OPERATING PROCESSES SIMULATION ISSUES ANALYSIS

ÀÍÀË²Ç ÎÑÎÁËÈÂÎÑÒÅÉ ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ  ÏÀËÈÂÍÈÕ ØÅÑÒÅÐÅÍÍÈÕ ÍÀÑÎÑÀÕ ÃÒÄ

ÀÍÀËÈÇ ÎÑÎÁÅÍÍÎÑÒÅÉ ÌÎÄÅËÈÐÎÂÀÍÈß ÏÐÎÖÅÑÑÎÂ Â ÒÎÏËÈÂÍÛÕ ØÅÑÒÅÐÅÍÍÛÕ ÍÀÑÎÑÀÕ ÃÒÄ

24–30

Åïèôàíîâ Ñ. Â.,
Ëè Öèöçå

ERROR ANALYSIS OF THERMOCOUPLE DYNAMIC PERFORMANCES EXPERIMENTAL DETERMINING IN ENGINE CONDITIONS USING STEP RESPONCE

ÀÍÀË²Ç ÏÎÕÈÁÎÊ ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÃÎ ÂÈÇÍÀ×ÅÍÍß ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÅÐÌÎÏÀÐÈ Â ÓÌÎÂÀÕ ÄÂÈÃÓÍÀ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÑÒÐÈÁÊÎÏÎIJÁÍÎÃÎ ÂÏËÈÂÓ

ÀÍÀËÈÇ ÏÎÃÐÅØÍÎÑÒÅÉ ÎÏÐÅÄÅËÅÍÈß ÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÀÐÀÌÅÒÐΠÒÅÐÌÎÏÀÐÛ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎ-ÐÀÑ×ÅÒÍÛÌ ÌÅÒÎÄÎÌ

31-40

Êîíñòðóêö³ÿ ³ ì³öí³ñòü àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê

Ïðèäîðîæíûé Ð. Ï.,
Øåðåìåòüåâ
À. Â.,
Çèíüêîâñêèé À. Ï.

INFLUENCE OF CREEP OF MATERIAL OF A HIGH PRESSURE NOZZLEVANES ON THEIR OPERABILITY

ÂÏËÈ ÏÎÂÇÓ×ÎÑÒ² ÌÀÒÅвÀËÓ ÍÀ ÐÎÁÎÒÎÇÄÀÒͲÑÒÜ ËÎÏÀÒÎÊ ÑÎÏËÎÂÎÃÎ ÀÏÀÐÀÒÓ ÒÓÐÁ²ÍÈ ÂÈÑÎÊÎÃÎ ÒÈÑÊÓ

ÂËÈßÍÈÅ ÏÎËÇÓ×ÅÑÒÈ ÌÀÒÅÐÈÀËÀ ÍÀ ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÜ ËÎÏÀÒÎÊ ÑÎÏËÎÂÎÃÎ ÀÏÏÀÐÀÒÀ ÒÓÐÁÈÍÛ ÂÛÑÎÊÎÃÎ ÄÀÂËÅÍÈß

41–46

Ñíåæíîé Ã. Â.,
Ñíåæíîé Â. Ë.

MAGNETOMETRIC METHOD FOR INVESTIGATION THE EFFECT OF CARBON AND NITROGEN ON THE CORROSION RESISTANCE OF AUSTENITIC CHROMIUM-NICKEL STEELS

ÌÀÃͲÒÎÌÅÒÐÈ×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÂÈÂ×ÅÍÍß ÂÏËÈÂÓ ÂÓÃËÅÖÞ ² ÀÇÎÒÓ ÍÀ ÊÎÐÎDzÉÍÓ ÒÐÈÂʲÑÒÜ ÀÓÑÒÅͲÒÍÈÕ ÕÐÎÌÎͲÊÅËÅÂÈÕ ÑÒÀËÅÉ

ÌÀÃÍÈÒÎÌÅÒÐÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÈÇÓ×ÅÍÈÞ ÂËÈßÍÈß ÓÃËÅÐÎÄÀ È ÀÇÎÒÀ ÍÀ ÊÎÐÐÎÇÈÎÍÍÓÞ ÑÒÎÉÊÎÑÒÜ ÀÓÑÒÅÍÈÒÍÛÕ ÕÐÎÌÎÍÈÊÅËÅÂÛÕ ÑÒÀËÅÉ

47–51

Êóõòèí Þ. Ï.,
Øàêàëî Ð. Þ.

REDUCING VIBRATION TENSION OF PAIRWISE SHROUDED BLADES OF TURBINE

ÇÍÈÆÅÍÍß Â²ÁÐÎÍÀÏÐÓÆÅÍÎÑÒ² ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÎÂÀÍÈÕ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁ²ÍÈ

ÑÍÈÆÅÍÈÅ ÂÈÁÐÎÍÀÏÐ߯ÅÍÍÎÑÒÈ ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÈÐÎÂÀÍÍÛÕ ÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÈÍÛ

52–58

Òåõíîëî㳿 âèðîáíèöòâà îá'ºêò³â àâ³àö³éíî-êîñì³÷íî¿ òåõí³êè

Àäæàìñêèé Ñ. Â.,
Êîíîíåíêî À. À.,
Ïîäîëüñêèé Ð. Â.

ÐROSPECTS FOR THE APPLICATION OF ADDITIVE TECHNOLOGIES IN AIRCRAFT AND ROCKET ENGINEERING

ÏÅÐÑÏÅÊÒÈÂÈ ÇÀÑÒÎÑÓÂÀÍÍß ÀÄÄÈÒÈÂÍÈÕ ÒÅÕÍÎËÎÃ²É Ó À²À-ÒÀ ÐÀÊÅÒÎÁÓÄÓÂÀÍÍß

ÏÅÐÑÏÅÊÒÈÂÛ ÏÐÈÌÅÍÅÍÈß ÀÄÄÈÒÈÂÍÛÕ ÒÅÕÍÎËÎÃÈÉ Â ÀÂÈÀ- È ÐÀÊÅÒÎÑÒÐÎÅÍÈÈ

59–65

Ïåäàø À. À.,
Êàñàé Ï. À.,
Êëî÷èõèí Â. Â.,
Øèëî Â. Ã.

STRUCTURE AND PROPERTIES OF SLM-MANUFACTURED PARTS AFTER LCF-TESTING

ÑÒÐÓÊÒÓÐÀ É ÂËÀÑÒÈÂÎÑÒ² ÄÅÒÀËÅÉ, ÙÎ ÎÒÐÈÌÀͲ ÑÅËÅÊÒÈÂÍÛÌ ËÀÇÅÐÍÈÌ ÑÏËÀÂËÅÍÍßÌ Ï²ÑËß ÂÈÏÐÎÁÓÂÀÍÍß ÍÀ ÌÀËÎÖÈÊËÎÂÓ ÂÒÎÌÓ

ÑÒÐÓÊÒÓÐÀ È ÑÂÎÉÑÒÂÀ ÄÅÒÀËÅÉ, ÏÎËÓ×ÅÍÍÛÕ ÑÅËÅÊÒÈÂÍÛÌ ËÀÇÅÐÍÛÌ ÑÏËÀÂËÅÍÈÅÌ ÏÎÑËÅ ÈÑÏÛÒÀÍÈß ÍÀ ÌÀËÎÖÈÊËÎÂÓÞ ÓÑÒÀËÎÑÒÜ

66–72

Âèøíåïîëüñêèé Å. Â.,
Ïàâëåíêî Ä. Â.,
Äâèðíûê ß. Â.

PREDICTED EFFECTS OF STRENGTHENING BY DIAMOND IRONING OF DETAILS OBTAINED BY SELECTIVE LASER SINTERING

ÏÐÎÃÍÎÇÎÂÀͲ ÅÔÅÊÒÈ Ç̲ÖÍÅÍÍß ÀËÌÀÇÍÈÌ ÂÈÏÐÀÑÎÂÓÂÀÍÍßÌ ÄÅÒÀËÅÉ ÎÒÐÈÌÀÍÈÕ ÇÀ ÄÎÏÎÌÎÃÎÞ ÑÅËÅÊÒÈÂÍÎÃÎ ËÀÇÅÐÍÎÃÎ ÑϲÊÀÍÍß

ÏÐÎÃÍÎÇÈÐÓÅÌÛÅ ÝÔÔÅÊÒÛ ÓÏÐÎ×ÍÅÍÈß ÀËÌÀÇÍÛÌ ÂÛÃËÀÆÈÂÀÍÈÅÌ ÄÅÒÀËÅÉ ÏÎËÓ×ÅÍÍÛÕ Ñ ÏÎÌÎÙÜÞ ÑÅËÅÊÒÈÂÍÎÃÎ ËÀÇÅÐÍÎÃÎ ÑÏÅÊÀÍÈß

73–82

²íôîðìàö³éí³ òåõíîëî㳿

Áóðÿ÷åíêî À. Ã.,
Áóðóíîâ Ä. Ñ.,
Ãðóäèíêèí Â. Ì.,
Òàðàíèøèí À. Î.

STAND IMITATOR OF THE ENGINE AS A UNIVERSAL MEANS OF ENSURING THE DEVELOPMENT AND TESTING OF REGULATORS

ÑÒÅÍÄ-IÌIÒÀÒÎÐ ÀÂÈÀÄÂÈÃÓÍÀ ßÊ ÓÍÈÂÅÐÑÀËÜÍÈÉ ÇÀÑIÁ ÇÀÁÅÇÏÅ×ÅÍÍß ÐÎÇÐÎÁÊÈ ÒÀ ÂÈÏÐÎÁÓÂÀÍÜ ÐÅÃÓËßÒÎÐIÂ

ÑÒÅÍÄ-ÈÌÈÒÀÒÎÐ ÀÂÈÀÄÂÈÃÀÒÅËß ÊÀÊ ÓÍÈÂÅÐÑÀËÜÍÎÅ ÑÐÅÄÑÒÂÎ ÎÁÅÑÏÅ×ÅÍÈß ÐÀÇÐÀÁÎÒÊÈ È ÈÑÏÛÒÀÍÈÉ ÐÅÃÓËßÒÎÐÎÂ

83–88

Åïèôàíîâ Ñ. Â.,
Çåëåíñêèé Ð. Ë.,
Áîíäàðåíêî À. Â.

RESEARCHING OF RELATIONS FORMING BETWEEN PARAMETERS OF TWO-SPOOL TURBOFAN DYNAMIC MODEL AND OPERATION MODE

ÄÎÑË²ÄÆÅÍÍß ÏÐÎÁËÅÌÈ ÔÎÐÌÓÂÀÍÍß ÇÀËÅÆÍÎÑÒ² ÏÀÐÀÌÅÒв ÄÈÍÀ̲×Íί ÌÎÄÅ˲ ÄÂÎÂÀËÜÍÎÃÎ ÒÐÄÄ Â²Ä ÐÅÆÈÌÓ ÐÎÁÎÒÈ

ÈÑÑËÅÄÎÂÀÍÈÅ ÏÐÎÁËÅÌÛ ÔÎÐÌÈÐÎÂÀÍÈß ÇÀÂÈÑÈÌÎÑÒÈ ÏÀÐÀÌÅÒÐΠÄÈÍÀÌÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÄÂÓÕÂÀËÜÍÎÃÎ ÒÐÄÄ ÎÒ ÐÅÆÈÌÀ ÐÀÁÎÒÛ

89–97

Tamargazin À.,
Pryimak L.

NEURAL NETWORK INTERPOLATION PARAMETERS OF A MULTI-MODE DYNAMIC MODEL OF THE AIRCRAFT ENGINE

ÍÅÉÐÎÌÅÐÅÆÅÂÀ ²ÍÒÅÐÏÎËßÖ²ß ÏÀÐÀÌÅÒв ÁÀÃÀÒÎÐÅÆÈÌÍί ÄÈÍÀ̲×Íί ÌÎÄÅ˲ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ

ÍÅÉÐÎÑÅÒÅÂÀß ÈÍÒÅÐÏÎËßÖÈß ÏÀÐÀÌÅÒÐΠÌÍÎÃÎÐÅÆÈÌÍÎÉ ÄÈÍÀÌÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß

98–104

Îãàíÿí È. Â.

MATHEMATICAL MODEL OF FUEL PUMP-REGULATOR OF HELICOPTER TURBO-SHAFT ENGINE

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÏÀËÈÂÍÎÃÎ ÍÀÑÎÑÀ-ÐÅÃÓËßÒÎÐÀ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÓÍÀ ÂÅÐÒÎËÜÎÒÀ

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÒÎÏËÈÂÍÎÃÎ ÍÀÑÎÑÀ-ÐÅÃÓËßÒÎÐÀ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÀÒÅËß ÂÅÐÒÎËÅÒÀ

105–112

Òîâêà÷ Ñ. Ñ.

APPROACH OF FUZZY CLUSTERING IN DISTRIBUTED INFORMATION SYSTEMS OF AVIATION ENGINES

ϲÄÕ²Ä ÍÅײÒÊί ÊËÀÑÒÅÐÈÇÀÖ²¯  ÐÎÇÏÎIJËÅÍÈÕ ²ÍÔÎÐÌÀÖ²ÉÍÈÕ ÑÈÑÒÅÌÀÕ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÏÎÄÕÎÄ ÍÅ×ÅÒÊÎÉ ÊËÀÑÒÅÐÈÇÀÖÈÈ Â ÐÀÑÏÐÅÄÅËÅÍÍÛÕ ÈÍÔÎÐÌÀÖÈÎÍÍÛÕ ÑÈÑÒÅÌÀÕ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

113–117

Âàðáàíåö Ð. À.,
Çàëîæ Â. È.,
Òàðàñåíêî Ò. Â.,
Áåëîóñîâà Ò. Ï.,
Åðûãàíîâ À. Â.

THE METHOD OF ANALYTICAL SYNCHRONIZATION OF THE WORKING PROCESS DATA MONITORING IN TRANSPORT DIESEL ENGINES OPERATING

ÌÅÒÎÄ ÀÍÀ˲ÒÈ×Íί ÑÈÍÕÐÎͲÇÀÖ²¯ ÄÀÍÈÕ ÌÎͲÒÎÐÈÍÃÓ ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÒÐÀÍÑÏÎÐÒÍÈÕ ÄÈÇÅ˲  ÅÊÑÏËÓÀÒÀÖ²¯

ÌÅÒÎÄ ÀÍÀËÈÒÈ×ÅÑÊÎÉ ÑÈÍÕÐÎÍÈÇÀÖÈÈ ÄÀÍÍÛÕ ÌÎÍÈÒÎÐÈÍÃÀ ÐÀÁÎ×ÅÃÎ ÏÐÎÖÅÑÑÀ ÒÐÀÍÑÏÎÐÒÍÛÕ ÄÈÇÅËÅÉ Â ÝÊÑÏËÓÀÒÀÖÈÈ

118–128

Ìèðãîðîä Â. Ô.,
Ãâîçäåâà ². Ì.

ESTIMATION OF POWER OF TREND CRITERIA

ÎÖ²ÍÊÀ ÏÎÒÓÆÍÎÑÒ² ÊÐÈÒÅв¯Â ÒÐÅÍÄÓ

ÎÖÅÍÊÀ ÌÎÙÍÎÑÒÈ ÊÐÈÒÅÐÈÅÂ ÒÐÅÍÄÀ

129–136

ʳÿíîâñüêèé Ì. Â.,
Öèâ³íäà Í. ².,
ϳê³ëüíÿê À. Â.,
Òðåòÿê Â. Â.

CHOICE OF MODELS FOR ADAPTIVE CONTROL BY RELIABILITY OF INDUSTRIAL EQUIPMENT «ON STATE»

ÂÈÁ²Ð ÌÎÄÅËÅÉ ÄËß ÀÄÀÏÒÈÂÍÎÃÎ ÊÅÐÓÂÀÍÍß ÍÀIJÉͲÑÒÞ ÏÐÎÌÈÑËÎÂÎÃÎ ÎÁËÀÄÍÀÍÍß «ÇÀ ÑÒÀÍÎÌ»

ÂÛÁÎÐ ÌÎÄÅËÅÉ ÄËß ÀÄÀÏÒÈÂÍÎÃÎ ÓÏÐÀÂËÅÍÈß ÍÀÄÅÆÍÎÑÒÜÞ ÏÐÎÌÛØËÅÍÍÎÃÎ ÎÁÎÐÓÄÎÂÀÍÈß «ÏÎ ÑÎÑÒÎßÍÈÞ»

137–145

Õðóëåâ À. Ý.,
Êëèìåíêî Â. Ã.

FEATURES OF COMPOSING AND APPLICATION OF LOGICAL METHODS FOR SEARCHING OF FAILURE CAUSES OF INTERNAL COMBUSTION PISTON ENGINES IN OPERATION

ÎÑÎÁËÈÂÎÑÒ² ÏÎÁÓÄÎÂÈ ÒÀ ÇÀÑÒÎÑÓÂÀÍÍß ËÎò×ÍÈÕ ÌÅÒÎIJ ÏÎØÓÊÓ ÏÐÈ×ÈÍ Â²ÄÌΠÏÎÐØÍÅÂÈÕ ÄÂÈÃÓͲ ÂÍÓÒвØÍÜÎÃÎ ÇÃÎÐÀÍÍß Â ÅÊÑÏËÓÀÒÀÖ²¯

ÎÑÎÁÅÍÍÎÑÒÈ ÏÎÑÒÐÎÅÍÈß È ÏÐÈÌÅÍÅÍÈß ËÎÃÈ×ÅÑÊÈÕ ÌÅÒÎÄΠÏÎÈÑÊÀ ÏÐÈ×ÈÍ ÎÒÊÀÇΠÏÎÐØÍÅÂÛÕ ÄÂÈÃÀÒÅËÅÉ ÂÍÓÒÐÅÍÍÅÃÎ ÑÃÎÐÀÍÈß Â ÝÊÑÏËÓÀÒÀÖÈÈ

146–157

²ÍÔÎÐÌÀÖ²ÉÍÅ ÏβÄÎÌËÅÍÍß

158

ÀËÔÀ²ÒÍÈÉ ÏÎÊÀÆ×ÈÊ

159

 

 

Øàíîâí³ ÷èòà÷³!

Íàóêîâî-òåõí³÷íèé æóðíàë «Àâ³àö³éíî-êîñì³÷íà òåõí³êà ³ òåõíîëîã³ÿ»

- âõîäèòü äî çàòâåðäæåíîãî ÄÀÊ Ïåðåë³êó íàóêîâèõ ôàõîâèõ âèäàíü Óêðà¿íè, â ÿêèõ ìîæóòü ïóáë³êóâàòèñÿ ðåçóëüòàòè äèñåðòàö³éíèõ ðîá³ò íà çäîáóòòÿ íàóêîâèõ ñòóïåí³â äîêòîðà ³ êàíäèäàòà íàóê çà ñïåö³àëüíîñòÿìè 113, 121, 122, 124, 126, 131, 132, 134, 141, 142, 151, 152, 153, 173, 272, 275 (íàêàç ÌÎÍ Óêðà¿íè ¹ 975 â³ä 11.07.2019 ð.);

- çáåð³ãàºòüñÿ â çàãàëüíîäåðæàâí³é ðåôåðàòèâí³é áàç³ äàíèõ «Óêðà¿í³êà íàóêîâà» òà ïóáë³êóºòüñÿ ó â³äïîâ³äíèõ òåìàòè÷íèõ ñåð³ÿõ óêðà¿íñüêîãî ðåôåðàòèâíîãî æóðíàëó «Äæåðåëî» (â³ëüíèé îíëàéíîâèé äîñòóï äî ðåñóðñ³â íà Web-ñåðâåð³ http://www.nbuv.gov.ua) (Óêðà¿íà) ,

- çáåð³ãàºòüñÿ â ðåôåðàòèâí³é áàç³ äàíèõ Âñåðîñ³éñüêîãî ³íñòèòóòó íàóêîâî¿ ³ òåõí³÷íî¿ ³íôîðìàö³¿ (²ͲҲ) Ðîñ³éñüêî¿ àêàäå쳿 íàóê ³ ïóáë³êóºòüñÿ ó â³äïîâ³äíèõ òåìàòè÷íèõ ñåð³ÿõ ÐÆ (â³ëüíèé îíëàéíîâèé äîñòóï äî ðåñóðñ³â íà Web-ñåðâåð³ http://www.viniti.ru) (Ðîñ³éñüêà Ôåäåðàö³ÿ ),

- âêëþ÷åíèé â ì³æíàðîäí³ á³áë³îìåòðè÷í³ ³ íàóêîìåòðè÷íèõ áàç äàíèõ: íàóêîâî¿ åëåêòðîííî¿ á³áë³îòåêè eLIBRARY.RU (Ðîñ³éñüêà Ôåäåðàö³ÿ); Index Copernicus (Ïîëüùà); DOAJ; CiteFactor; Academic Keys; Infobase Index; WordCat; Google Scholar.

 

Åëåêòðîííèé âàð³àíò æóðíàëó ðîçì³ùåíèé íà ñàéò³ http://nti.khai.edu/ojs/index.php/aktt