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 8(168). – 172 ñ.

ISSN: 1727-7337 (Print)2663-2217 (Online). ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2020. – ¹ 8(168). – 172 ñ.

ISSN: 1727-7337 (Print)2663-2217 (Online). AEROSPACE TECHNIC AND TECHNOLOGY. – 2020. – No. 8(168). – 172 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.,
Øìûðåâ Â. Ô.,
Ðÿáêîâ Â. È.

THE PROVISION OF COMPLETE SUPERIORITY OF TACTICAL MTA AN-188

ÄÎÑßÃÍÅÍÍß ÏÅÐÅÂÀÃÈ ÀÍ-188 ÑÅÐÅÄ ÎÏÅÐÀÒÈÂÍÎ-ÒÀÊÒÈ×ÍÈÕ Â²ÉÑÜÊÎÂÎ-ÒÐÀÍÑÏÎÐÒÍÈÕ Ë²ÒÀʲÂ

ÄÎÑÒÈÆÅÍÈÅ ÏÐÅÈÌÓÙÅÑÒÂÀ ÀÍ-188 ÑÐÅÄÈ ÎÏÅÐÀÒÈÂÍΖÒÀÊÒÈ×ÅÑÊÈÕ ÂÎÅÍÍÎ-ÒÐÀÍÑÏÎÐÒÍÛÕ ÑÀÌÎËÅÒÎÂ

5–11

Äìèòð³ºâ Ñ. Î.,
Ñóðîâöåâ Î. Þ.

ALGORITHM OF INTEGRATION OF THE POWER PLANT OF MEDIUM-RANGE PASSENGER PLANES

ÀËÃÎÐÈÒÌ ²ÍÒÅÃÐÀÖ²¯ ÑÈËÎÂί ÓÑÒÀÍÎÂÊÈ ÏÀÑÀÆÈÐÑÜÊÈÕ Ë²ÒÀʲ ÑÅÐÅÄÍÜί ÄÀËÜÍÎÑÒ²

ÀËÃÎÐÈÒÌ ÈÍÒÅÃÐÀÖÈÈ ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÈ ÏÀÑÑÀÆÈÐÑÊÈÕ ÑÀÌÎËÅÒÎÂ ÑÐÅÄÍÅÉ ÄÀËÜÍÎÑÒÈ

12–18

Çàéöåâ Á. Ô.,
Ïðîòàñîâà Ò.
 Â.,
Êëèìåíêî Ä.
 Â.,
Àêèìîâ Ä.
 Â.,
Ñèðåíêî Â.
 Í.

DYNAMIC ANALYSIS OF A COMPOSITE ROCKET DOME DURING SEPARATING TAKING INTO ACCOUNT STRUCTURE DELAMINATING

ÄÈÍÀ̲×ÍÈÉ ÀÍÀË²Ç ÊÎÌÏÎÇÈÒÍÎÃÎ ÎÁÒ²×ÍÈÊÀ ÐÀÊÅÒÈ ÏÐÈ Â²ÄIJËÅÍͲ Ç ÓÐÀÕÓÂÀÍÍßÌ ÐÎÇØÀÐÓÂÀÍÍß ÑÒÐÓÊÒÓÐÈ

ÄÈÍÀÌÈ×ÅÑÊÈÉ ÀÍÀËÈÇ ÊÎÌÏÎÇÈÒÍÎÃÎ ÎÁÒÅÊÀÒÅËß ÐÀÊÅÒÛ ÏÐÈ ÎÒÄÅËÅÍÈÈ Ñ Ó×ÅÒÎÌ ÐÀÑÑËÎÅÍÈß ÑÒÐÓÊÒÓÐÛ

19–26

Òåîð³ÿ ³ ðîáî÷³ ïðîöåñè àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê

Ãîðáåíêî Ã. À.,
Òóðíà Ð. Þ.,
Îðëîâ Ð. Ñ.,
Ðîãîâîé Å. Ý.

HEAT TRANSFER CAPACITY OF METAL MESH WICK

ÒÅÏËÎÒÐÀÍÑÏÎÐÒÍÀ ÇÄÀÒͲÑÒÜ ¥ÍÎÒÓ Ç ÌÅÒÀËÅÂÈÕ Ñ²ÒÎÊ

ÒÅÏËÎÒÐÀÍÑÏÎÐÒÍÀß ÑÏÎÑÎÁÍÎÑÒÜ ÔÈÒÈËß ÈÇ ÌÅÒÀËËÈ×ÅÑÊÈÕ ÑÅÒÎÊ

27–33

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

SELECTION AND JUSTIFICATION OF THE GRID GENERATION METHOD FOR FLOW SIMULATION IN A GAS TURBINE ENGINE FAN

ÂÈÁ²Ð ² ÎÁ¥ÐÓÍÒÓÂÀÍÍß ÌÅÒÎÄÓ ÃÅÍÅÐÀÖ²¯ ѲÒÊÈ ÄËß ÌÎÄÅËÞÂÀÍÍß ÒÅײ¯ Ó ÂÅÍÒÈËßÒÎв ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ

ÂÛÁÎÐ È ÎÁÎÑÍÎÂÀÍÈÅ ÌÅÒÎÄÀ ÃÅÍÅÐÀÖÈÈ ÑÅÒÊÈ ÄËß ÌÎÄÅËÈÐÎÂÀÍÈß ÒÅ×ÅÍÈß Â ÂÅÍÒÈËßÒÎÐÀÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

34–40

Êîíñòðóêö³ÿ ³ ì³öí³ñòü àâ³àö³éíèõ äâèãóí³â ³ åíåðãîóñòàíîâîê

dzíüêîâñüêèé À. Ï.,
Ìåðêóëîâ Â. Ì.,
Òîêàð ². Ã.,
Äåðêà÷ Î. Ë.,
Øàêàëî Ð. Þ.

RESEARCH OF THE INFLUENCE OF PEN FLEXIBILITY ON OPTIMUM REQUIREMENTS LINKINGS OF SHELVES PAIRWISE SHROUDED BLADES OF TURBINES

ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÃÍÓ×ÊÎÑÒ² ÏÅÐÀ ÍÀ ÎÏÒÈÌÀËÜͲ ÓÌÎÂÈ ÑÏÐ߯ÅÍÍß ÏÎËÈÖÜ ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÎÂÀÍÈÕ ËÎÏÀÒÎÊ ÒÓÐÁ²Í

ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÃÈÁÊÎÑÒÈ ÏÅÐÀ ÍÀ ÎÏÒÈÌÀËÜÍÛÅ ÓÑËÎÂÈß ÑÎÏÐ߯ÅÍÈß ÏÎËÎÊ ÏÎÏÀÐÍÎ ÁÀÍÄÀÆÈÐÎÂÀÍÍÛÕ ËÎÏÀÒÎÊ ÒÓÐÁÈÍ

41–49

Òêà÷ Ì. Ð.,
Ìîðãóí À.,
Çîëîòîé Þ. Ã.,
Ïðîñêóðèí À. Þ.,
Ãàëûíêèí Þ. Í.

FREE VIBRATIONS OF GAS TURBINE ENGINE AXIAL COMPRESSOR BLADES

²ËÜͲ ÊÎËÈÂÀÍÍß ËÎÏÀÒÎÊ ÎÑÜÎÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ

ÑÂÎÁÎÄÍÛÅ ÊÎËÅÁÀÍÈß ËÎÏÀÒÎÊ ÎÑÅÂÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß

50–60

Äîí÷åíêî Â. Â.,
Êðàâ÷åíêî È. Ô.

THE EXPERIMENTAL-RATED METHOD OF STYDYING OF WIDE-CHORD FAN OF THE AIRCRAFT ENGINE FOR THE ABSENCE OF FLUTTER

ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÈÉ ÌÅÒÎÄ ÄÎÑË²ÄÆÅÍÍß ØÈÐÎÊÎÕÎÐÄÍÎÃÎ ÂÅÍÒÈËßÒÎÐÀ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ²ÄÑÓÒͲÑÒÜ ÀÂÒÎÊÎËÈÂÀÍÜ

ÐÀÑ×ÅÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÉ ÌÅÒÎÄ ÈÑÑËÅÄÎÂÀÍÈß ØÈÐÎÊÎÕÎÐÄÍÎÃÎ ÂÅÍÒÈËßÒÎÐÀ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀ ÎÒÑÓÒÑÒÂÈÅ ÀÂÒÎÊÎËÅÁÀÍÈÉ

61–66

Ôèëèïêîâñêèé Ñ. Â.,
×èãðèí Â. Ñ.,
Òîïàë Í. Ñ.,
Ôèëèïêîâñêàÿ Ë. À.
 

RESEARCH METHOD OF THE AIRCRAFT ENGINE HOUSING VIBRATION WHEN THE FAN BLADE ABRUPTION

ÌÅÒÎÄ ÄÎÑË²ÄÆÅÍÍß Â²ÁÐÀÖ²¯ ÊÎÐÏÓÑÓ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ ÏÐÈ Â²ÄÐȲ ËÎÏÀÒÊÈ ÂÅÍÒÈËßÒÎÐÀ

ÌÅÒÎÄ ÈÑÑËÅÄÎÂÀÍÈß ÂÈÁÐÀÖÈÈ ÊÎÐÏÓÑÀ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÏÐÈ ÎÒÐÛÂÅ ËÎÏÀÒÊÈ ÂÅÍÒÈËßÒÎÐÀ

67–72

Ïåòóõîâ È. È.,
Ìèõàéëåíêî Ò. Ï.,
Áðóíàê À. À.,
Åïèôàíîâ Ñ. Â.,
Êîâàë¸â À. Â.,
Øåâ÷óê Î. Â.,
Òèõîìèðîâ Â. Â.

PECULIARITIES OF EXPERIMENTAL D ATA PROCESSING IN DETERMINING THE HEAT TRANSFER COEFFICIENT IN THE BEARING CHAMBER OF GTE

ÎÑÎÁËÈÂÎÑÒ² ÎÁÐÎÁÊÈ ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÈÕ ÄÀÍÈÕ ÏÐÈ ÂÈÇÍÀ×ÅÍͲ ÊÎÅÔ²Ö²ªÍÒÀ ÒÅÏËβÄÄÀײ  ÌÀÑËßÍ²É ÏÎÐÎÆÍÈͲ ÎÏÎÐÈ ÃÒÄ

ÎÑÎÁÅÍÍÎÑÒÈ ÎÁÐÀÁÎÒÊÈ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÕ ÄÀÍÍÛÕ ÏÐÈ ÎÏÐÅÄÅËÅÍÈÈ ÊÎÝÔÔÈÖÈÅÍÒÀ ÒÅÏËÎÎÒÄÀ×È Â ÌÀÑËßÍÎÉ ÏÎËÎÑÒÈ ÎÏÎÐÛ ÃÒÄ

73–81

Èâ÷åíêî Ä. Â.,
Ìåðêóëîâ Â. Ì.,
Ñìåòàíêèíà Í. Â.

THE DEVELOPMENT OF THE BIRD-IMPACTOR MODEL FOR MATHEMATICAL MODELING OF TURBOFAN ENGINE PARTS DAMAGE PROCESSES

ÐÎÇÐÎÁÊÀ ÌÎÄÅ˲ ÏÒÀÕÀ-ÓÄÀÐÍÈÊÀ ÄËß ÌÀÒÅÌÀÒÈ×ÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ÏÎØÊÎÄÆÅÍÍß ÄÅÒÀËÅÉ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ

ÐÀÇÐÀÁÎÒÊÀ ÌÎÄÅËÈ ÏÒÈÖÛ-ÓÄÀÐÍÈÊÀ ÄËß ÌÀÒÅÌÀÒÈ×ÅÑÊÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÏÐÎÖÅÑÑΠÏÎÂÐÅÆÄÅÍÈß ÄÅÒÀËÅÉ ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß

82–90

Ãóñåâ Þ. À.

PARAMETRIC IDENTIFICATION AND OPTIMIZATION OF HIGH-TEMPERATURE TENSORESISTORS

ÏÀÐÀÌÅÒÐÈ×ÍÀ ²ÄÅÍÒÈÔ²ÊÀÖ²ß ² ÎÏÒÈ̲ÇÀÖ²ß ÂÈÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÈÕ ÒÅÐÌÎÐÅÇÈÑÒÎвÂ

ÏÀÐÀÌÅÒÐÈ×ÅÑÊÀß ÈÄÅÍÒÈÔÈÊÀÖÈß È ÎÏÒÈÌÈÇÀÖÈß ÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÛÕ ÒÅÍÇÎÐÅÇÈÑÒÎÐÎÂ

91–99

Íàçèí Â. È.

INFLUENCE MASS OF THE RINGS, RESILIENTLY SET ON DISK, ON DYNAMIC DESCRIPTIONS OF HYDROSTATODYNAMIC BEARING OF THE DOUBLED TYPE

ÐÅÊÎÌÅÍÄÀÖ²¯ ÙÎÄÎ ÏÐÎÅÊÒÓÂÀÍÍß Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÈÕ Ï²ÄØÈÏÍÈʲ ÊÎÂÇÀÍÍß ÇÄÂΪÍÎÃÎ ÒÈÏÓ

ÐÅÊÎÌÅÍÄÀÖÈÈ ÏÎ ÏÐÎÅÊÒÈÐÎÂÀÍÈÞ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÎÄØÈÏÍÈÊΠÑÊÎËÜÆÅÍÈß ÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ

100–105

Òàðàñåíêî À. À.,
Òàðàñåíêî À. È.
 

EQUATIONS OF SPATIAL MOTION OF A SOLID BODY WITH MOLDABLE FASTENING TO THE FOUNDATION (THE TASK OF DEPRECIATION IN SPACE)

вÂÍßÍÍß ÏÐÎÑÒÎÐÎÂÎÃÎ ÐÓÕÓ ÒÂÅÐÄÎÃÎ Ò²ËÀ Ç ÏÎÄÀÒËÈÂÈÌ ÊвÏËÅÍÍßÌ ÄÎ ÔÓÍÄÀÌÅÍÒÓ (ÇÀÂÄÀÍÍß ÀÌÎÐÒÈÇÀÖ²¯  ÏÐÎÑÒÎв)

ÓÐÀÂÍÅÍÈß ÏÐÎÑÒÐÀÍÑÒÂÅÍÍÎÃÎ ÄÂÈÆÅÍÈß ÒÂÅÐÄÎÃÎ ÒÅËÀ Ñ ÏÎÄÀÒËÈÂÛÌ ÊÐÅÏËÅÍÈÅÌ Ê ÔÓÍÄÀÌÅÍÒÓ (ÇÀÄÀ×À ÀÌÎÐÒÈÇÀÖÈÈ Â ÏÐÎÑÒÐÀÍÑÒÂÅ)

106–110

Ðèìàðåíêî ª. Î.

CURRENT STATE OF THE PROBLEM OF THE DEVELOPMENT OF ACOUSTIC LINERS FOR GAS-TURBINE ENGINES

ÑÓ×ÀÑÍÈÉ ÑÒÀÍ ÏÐÎÁËÅÌÈ ÐÎÇÐÎÁÊÈ ÇÂÓÊÎÏÎÃËÈÍÀÞ×ÈÕ ÊÎÍÑÒÐÓÊÖ²É ÄËß ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲÂ

ÑÎÂÐÅÌÅÍÍÎÅ ÑÎÑÒÎßÍÈÅ ÏÐÎÁËÅÌÛ ÐÀÇÐÀÁÎÒÊÈ ÇÂÓÊÎÏÎÃËÎÙÀÞÙÈÕ ÊÎÍÑÒÐÓÊÖÈÉ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

111–120

Ìîðîçîâ À. Â.

NUMERICAL DETERMINATION OF EFFECTIVE ELASTIC CHARACTERISTICS OF THREE-DIMENSIONAL FIBER COMPOSITE MATERIAL

×ÈÑÅËÜÍÅ ÂÈÇÍÀ×ÅÍÍß ÅÔÅÊÒÈÂÍÈÕ ÏÐÓÆÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÐÈÂÈ̲ÐÍÎÀÐÌÎÂÀÍÎÃÎ ÂÎËÎÊÍÈÑÒÎÃÎ ÊÎÌÏÎÇÈÖ²ÉÍÎÃÎ ÌÀÒÅвÀËÓ

×ÈÑËÅÍÍÎÅ ÎÏÐÅÄÅËÅÍÈÅ ÝÔÔÅÊÒÈÂÍÛÕ ÓÏÐÓÃÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒШÕÌÅÐÍÎÀÐÌÈÐÎÂÀÍÍÎÃÎ ÊÎÌÏÎÇÈÖÈÎÍÍÎÃÎ ÌÀÒÅÐÈÀËÀ

121–129

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

Ìàêîâñêèé Ñ. Ã.,
Ëóêèíîâ Â. Â.,
Êëî÷èõèí Â. Â.,
Øàëîìååâ Â. À.,
Øåéêî Ñ. Ï.

INOCULATION OF ML5 MAGNESIUM ALLOY WITH CARBON NANOPOWDER

ÌÎÄÈÔIÊÓÂÀÍÍß ÌÀÃÍIªÂÎÃÎ ÑÏËÀÂÓ ÌË5 ÍÀÍÎÏÎÐÎØÊÎÌ ÂÓÃËÅÖÞ

ÌÎÄÈÔÈÖÈÐÎÂÀÍÈÅ ÌÀÃÍÈÅÂÎÃÎ ÑÏËÀÂÀ ÌË5 ÍÀÍÎÏÎÐÎØÊÎÌ ÓÃËÅÐÎÄÀ

130–135

Åâäîêèìåíêî Þ. È.,
Ãóñàðîâà È. À.,
Ôðîëîâ Ã. À.,
Êèñåëü Â. Ì.,
Áó÷àêîâ Ñ. Â.

THERMOPHYSICAL CHARACTERISTICS AND THERMOEROSION RESISTANCE OF CERAMIC MATERIAL BASED ON BORON CARBIDE

ÒÅÏËÎÔ²ÇÈ×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ² ÒÅÐÌÎÅÐÎDzÉÍÀ ÑÒ²ÉʲÑÒÜ ÊÅÐÀ̲×ÍÎÃÎ ÌÀÒÅвÀËÓ ÍÀ ÎÑÍβ ÊÀÐÁ²ÄÓ ÁÎÐÓ

ÒÅÏËÎÔÈÇÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ È ÒÅÐÌÎÝÐÎÇÈÎÍÍÀß ÑÒÎÉÊÎÑÒÜ ÊÅÐÀÌÈ×ÅÑÊÎÃÎ ÌÀÒÅÐÈÀËÀ ÍÀ ÎÑÍÎÂÅ ÊÀÐÁÈÄÀ ÁÎÐÀ

136–145

Òðåòÿê Â. Â.

MATION OF FORM OF SPATIAL SHELLS BY METHOD OF EXPLOSIVE STAMPING

ÔÎÐÌÎÓÒÂÎÐÅÍÍß ÏÐÎÑÒÎÐÎÂÈÕ ÎÁÎËÎÍÎÊ ÇÀ ÄÎÏÎÌÎÃÎÞ ÂÈÁÓÕÎÂÎÃÎ ØÒÀÌÏÓÂÀÍÍß

ÔÎÐÌÎÎÁÐÀÇÎÂÀÍÈÅ ÏÐÎÑÒÐÀÍÑÒÂÅÍÍÛÕ ÎÁÎËÎ×ÅÊ ÌÅÒÎÄÎÌ ÂÇÐÛÂÍÎÉ ØÒÀÌÏÎÂÊÈ

146–152

Âîëêîâ À. Î.,
Øîð³íîâ Î. Â.,
Äîëìàòîâ À. ².,
Ìàðêîâè÷ Ñ. ª.

SIMULATION OF TWO-PHASE FLOW IN COLD GAS-DYNAMIC SPRAYING

ÌÎÄÅËÞÂÀÍÍß ÄÂÎÔÀÇÍÎÃÎ ÏÎÒÎÊÓ ÏÐÈ ÕÎËÎÄÍÎÌÓ ÃÀÇÎÄÈÍÀ̲×ÍÎÌÓ ÍÀÏÈËÞÂÀÍͲ

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÄÂÓÕÔÀÇÍÎÃÎ ÏÎÒÎÊÀ ÏÐÈ ÕÎËÎÄÍÎÌ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÌ ÍÀÏÛËÅÍÈÈ

153-159

²íôîðìàö³éí³ òåõíîëî㳿

Ðàí÷åíêî Ã. Ñ.,
Áóðÿ÷åíêî À. Ã.,
Ãðóäèíêèí Â. Ì.,
Äàíèëîâ Â. Â.

BASIC MODEL OF THE AIRCRAFT ENGINE REGULATOR AND ITS MODIFICATIONS

ÁÀÇÎÂÅ ÂÈÊÎÍÀÍÍß ÐÅÃÓËßÒÎÐÀ ÀÂIÀÄÂÈÃÓÍÀ ÒÀÉÎÃÎ ÌÎÄÈÔÈÊÀÖ²¯

ÁÀÇÎÂÎÅ ÈÑÏÎËÍÅÍÈÅ ÐÅÃÓËßÒÎÐÀ ÀÂÈÀÄÂÈÃÀÒÅËß È ÅÃÎ ÌÎÄÈÔÈÊÀÖÈÈ

160–165

Òîìàøåâñüêèé Î. Â.,
Ñí³æíîé Ã. Â.

STUDY OF INDICATORS OF EFFICIENCY OF OPERATION OF MEANS OF MEASUREMENTS BY THE METHOD OF COMPUTER SIMULATION

ÄÎÑË²ÄÆÅÍÍß ÏÎÊÀÇÍÈÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² ÅÊÑÏËÓÀÒÀÖ²¯ ÇÀÑÎÁ²Â ÂÈ̲ÐÞÂÀËÜÍί ÒÅÕͲÊÈ ÌÅÒÎÄÎÌ ÊÎÌÏ’ÞÒÅÐÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß

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166–169

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170

ÀËÔÀ²ÒÍÈÉ ÏÎÊÀÆ×ÈÊ

171

 

 

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