Íàöèîíàëüíûé àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé èíñòèòóò”

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 5 (112). – 114 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 5 (112). – 114 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2014. – ¹ 5 (112). – 114 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè (article title)

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(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Íàðûæíûé À. Ã.,
Êóöåíêî Þ. Í.,
Ãðîì Ì. Â.,
Ñòåïàíåíêî Ä. Ð.

THE THERMOMECHANICAL MODEL OF CUTTING PROCESS BY CUTTING TOOLS WITH THE WEAR-RESISTANT COATING

ÒÅÐÌÎÌÅÕÀͲ×ÍÀ ÌÎÄÅËÜ ÏÐÎÖÅÑÓ Ð²ÇÀÍÍß Ð²ÆÓ×ÈÌ ²ÍÑÒÐÓÌÅÍÒÎÌ Ç² ÇÍÎÑÎÑÒ²ÉÊÈÌ ÏÎÊÐÈÒÒßÌ

ÒÅÐÌÎÌÅÕÀÍÈ×ÅÑÊÀß ÌÎÄÅËÜ ÏÐÎÖÅÑÑÀ ÐÅÇÀÍÈß ÐÅÇÖÎÌ Ñ ÈÇÍÎÑÎÑÒÎÉÊÈÌ ÏÎÊÐÛÒÈÅÌ

4–10
(7)

Õîäüêî À. À.

CHOOSING A METAL PLASTICITY MODEL FOR NUMERICAL SIMULATION OF THE HYDRODYNAMIC FORMING PROCESS

ÎÑÎÁËÈÂÎÑÒ² ÂÈÁÎÐÓ ÌÎÄÅ˲ ÏËÀÑÒÈ×ÍÎÑÒ² ÌÅÒÀËÓ ÄÅÔÎÐÌÓªÌί ÇÀÃÎÒÎÂÊÈ ÏÐÈ ×ÈÑÅËÜÍÎÌÓ ÄÎÑË²ÄÆÅÍͲ ÏÐÎÖÅÑÓ Ã²ÄÐÎÄÈÍÀ̲×Íί ØÒÀÌÏÎÂÊÈ

ÎÑÎÁÅÍÍÎÑÒÈ ÂÛÁÎÐÀ ÌÎÄÅËÈ ÏËÀÑÒÈ×ÍÎÑÒÈ ÌÅÒÀËËÀ ÄÅÔÎÐÌÈÐÓÅÌÎÉ ÇÀÃÎÒÎÂÊÈ ÏÐÈ ×ÈÑËÅÍÍÎÌ ÈÑÑËÅÄÎÂÀÍÈÈ ÏÐÎÖÅÑÑÀ ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÎÉ ØÒÀÌÏÎÂÊÈ

11–24
(14)

Ëÿêóí Ñ. Ô.,
Þðêåâè÷ Â. Å.

COMPUTATION ALGORITHM OF CONTROL PROGRAM ON TRIHEDRAL ANGLE PROCESSING AT CNC MACHINES

ÀËÃÎÐÈÒÌ ÐÎÇÐÀÕÓÍÊÓ ÊÅÐÓÞ×ί ÏÐÎÃÐÀÌÈ Ç ÎÁÐÎÁÊÈ ÒÐÈÃÐÀÍÍÎÃÎ ÊÓÒÀ ÍÀ ÂÅÐÑÒÀÒÀÕ Ç ×ÏÊ

ÀËÃÎÐÈÒÌ ÐÀÑ×ÅÒÀ ÓÏÐÀÂËßÞÙÅÉ ÏÐÎÃÐÀÌÌÛ ÏÎ ÎÁÐÀÁÎÒÊÅ ÒÐÅÕÃÐÀÍÍÎÃÎ ÓÃËÀ ÍÀ ÑÒÀÍÊÀÕ Ñ ×ÏÓ

25–32
(8)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ìåõîíîøèí Þ. Ã.,
×èæóõèí Â. Í.,
Èâàíîâ Ï. È.,
Èâàíîâ Ð. Ï.

PROBLEMATIC ISSUES OF THE DESIGNING OF AEROSPACE PARACHUTE SYSTEM

ÏÐÎÁËÅÌͲ ÏÈÒÀÍÍß ÏÐÎÅÊÒÓÂÀÍÍß ÏβÒÐßÍÎ-ÊÎÑ̲×Íί ÏÀÐÀØÓÒÍί ÑÈÑÒÅÌÈ

ÏÐÎÁËÅÌÍÛÅ ÂÎÏÐÎÑÛ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÏÀÐÀØÞÒÍÎÉ ÑÈÑÒÅÌÛ

33–39
(7)

Àâðàìîâ Ê. Â.,
Ìîðà÷êîâñêèé Î. Ê.,
Òîíêîíîæåíêî À. Ì.,
Êîæàðèí Â. Þ.,
Äåãòÿðåíêî Ï. Ã.  

NUMERICAL ANALYSIS OF ROCKETS TANKS BREAKING LOADS

×ÈÑÅËÜÍÈÉ ÀÍÀË²Ç ÐÓÉͲÂÍÈÕ ÍÀÂÀÍÒÀÆÅÍÜ ÎÁÐÅÁÐÅÍÈÕ ÁÀʲ ÐÀÊÅÒÎÍÎѲ¯Â

×ÈÑËÅÍÍÛÉ ÀÍÀËÈÇ ÐÀÇÐÓØÀÞÙÈÕ ÍÀÃÐÓÇÎÊ ÎÐÅÁÐÅÍÍÛÕ ÁÀÊΠÐÀÊÅÒÎÍÎÑÈÒÅËÅÉ

40–46
(7)

Íèêîëàåâ À. Ã.,
Òàí÷èê Å. À.

NEW addition theoremS OF basic solutionS of the Lame equation for prolate spheroids and their application to modeling POROUS MATERIAL

Íβ òåîðåìè äîäàâàííÿ ÁÀÇÈÑÍÈÕ ÐÎÇÂ’ßÇʲ вÂÍßÍÍß ËÀÌÅ äëÿ âèòÿãíóòèõ ñôåðî¿ä³Â ÒÀ ¯Õ ÇÀÑÒÎÑÓÂÀÍÍß äî ìîäåëþâàííÿ ïîðèñòîãî ìàòåð³àëó

ÍÎÂÛÅ ÒÅÎÐÅÌÛ ÑËÎÆÅÍÈß ÁÀÇÈÑÍÛÕ ÐÅØÅÍÈÉ ÓÐÀÂÍÅÍÈß ËÀÌÅ ÄËß ÂÛÒßÍÓÒÛÕ ÑÔÅÐÎÈÄÎÂ È ÈÕ ÏÐÈÌÅÍÅÍÈÅ Ê ÌÎÄÅËÈÐÎÂÀÍÈÞ ÏÎÐÈÑÒÎÃÎ ÌÀÒÅÐÈÀËÀ

47–55
(9)

Àìáðîæåâè÷ À. Â.,
Ãðèùåíêî À. Â.,
Êîðíåâ À. Â.,
Ìèãàëèí Ê. Â.,
Ñåðåäà Â. À.

CIRCULATION PRINCIPLE OF TRAJECTORY SUPPORT VIA INTEGRATION OF EJECTOR RAM-JET ENGINE INTO THE FLYING WING

ÖÈÐÊÓËßÖ²ÉÍÈÉ ÏÐÈÍÖÈÏ ÒÐÀªÊÒÎÐÍί ϲÄÒÐÈÌÊÈ ÇÀ ÐÀÕÓÍÎÊ ²ÍÒÅÃÐÀÖ²¯ ÅÆÅÊÒÎÐÍÎÃÎ ÏÐßÌÎÒÎ×ÎÃÎ ÄÂÈÃÓÍÀ  ˲ÒÀÞ×Å ÊÐÈËÎ

ÖÈÐÊÓËßÖÈÎÍÍÛÉ ÏÐÈÍÖÈÏ ÒÐÀÅÊÒÎÐÍÎÃÎ ÏÎÄÄÅÐÆÀÍÈß ÇÀ Ñ×ÅÒ ÈÍÒÅÃÐÀÖÈÈ ÝÆÅÊÒÎÐÍÎÃÎ ÏÐßÌÎÒÎ×ÍÎÃÎ ÄÂÈÃÀÒÅËß Â ËÅÒÀÞÙÅÅ ÊÐÛËÎ

56–63
(6)

Ôîìè÷åâ Ï. À.,
Ìàíäçþê Ñ. Ô.,
Ëåäîâñêèõ È. Â.

FINITE ELEMENT METHOD APLICATION IN THE PRE-CALIBRATION STAGE OF AN AIRPLANE SWEPTWING DISSECTED SECTIONS

ÇÀÑÒÎÑÓÂÀÍÍß ÌÅÒÎÄÓ ÑʲÍ×ÅÍÈÕ ÅËÅÌÅÍҲ ÍÀ ÅÒÀϲ ÏÎÏÅÐÅÄÍÜί ÊÀ˲ÁÐÎÂÊÈ ÏÐÅÏÀÐÎÂÀÍÈÕ ÏÅÐÅвDz ÑÒвËÎÏÎIJÁÍÎÃÎ ÊÐÈËÀ ˲ÒÀÊÀ

ÏÐÈÌÅÍÅÍÈÅ ÌÅÒÎÄÀ ÊÎÍÅ×ÍÛÕ ÝËÅÌÅÍÒΠÍÀ ÝÒÀÏÅ ÏÐÅÄÂÀÐÈÒÅËÜÍÎÉ ÒÀÐÈÐÎÂÊÈ ÏÐÅÏÀÐÈÐÎÂÀÍÍÛÕ ÑÅ×ÅÍÈÉ ÑÒÐÅËÎÂÈÄÍÎÃÎ ÊÐÛËÀ ÑÀÌÎËÅÒÀ

64–69
(6)

Õàëèëîâ Ñ. À.,
Ìèíòþê Â. Á.,
Òêà÷åíêî Ä. À.,
Êîïû÷êî Â. Â.

BIHARMONIC OPERATOR OWN SPECTRUM IN A RECTANGLE AT THE MAIN BOUNDARY CONDITIONS

ÂËÀÑÍÈÉ ÑÏÅÊÒÐ Á²ÃÀÐÌÎͲ×ÍÎÃÎ ÎÏÅÐÀÒÎÐÀ Ó ÏÐßÌÎÊÓÒÍÈÊÓ ÏÐÈ ÃÎËÎÂÍÈÕ ÊÐÀÉÎÂÈÕ ÓÌÎÂÀÕ

ÑÎÁÑÒÂÅÍÍÛÉ ÑÏÅÊÒÐ ÁÈÃÀÐÌÎÍÈ×ÅÑÊÎÃÎ ÎÏÅÐÀÒÎÐÀ  ÏÐßÌÎÓÃÎËÜÍÈÊÅ ÏÐÈ ÃËÀÂÍÛÕ ÊÐÀÅÂÛÕ ÓÑËÎÂÈßÕ

70–78
(9)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Êðèâîõàòüêî È. Ñ.,
Ñóõîâ Â. Â.

AERODYNAMIC PERFORMANCE DEFINITION OF UAV WITH COMPLEX PLANFORM WING AT LOW REYNOLDS NUMBER

ÂÈÇÍÀ×ÅÍÍß ÀÅÐÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ë²ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ Ç ÊÐÈËÎÌ ÑÊËÀÄÍί ÔÎÐÌÈ Â ÏËÀͲ ÏÐÈ ÍÈÇÜÊÈÕ ×ÈÑËÀÕ ÐÅÉÍÎËÜÄÑÀ

ÎÏÐÅÄÅËÅÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ Ñ ÊÐÛËÎÌ ÑËÎÆÍÎÉ ÔÎÐÌÛ Â ÏËÀÍÅ ÏÐÈ ÍÈÇÊÈÕ ×ÈÑËÀÕ ÐÅÉÍÎËÜÄÑÀ

79–85
(7)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Áîéêî Ë. Ã.,
ĸìèí À. Å.,
Ìàêñèìîâ Þ. Ï.,
Àõòåìåíêî Þ. Ô.,
Êàëþæíàÿ Â. À.

GTE MULTISTAGE AXIAL COMPRESSOR SUMMARY PERFORMANCES AND FLOW FEATURES ANALYSIS

ÀÍÀË²Ç ÎÑÎÁËÈÂÎÑÒÅÉ ÒÅײ¯ ÒÀ ÑÓÌÀÐÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÁÀÃÀÒÎÑÒÓÏÅÍÅÂÎÃΠ²ÑÜÎÂÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÃÒÄ

ÀÍÀËÈÇ ÎÑÎÁÅÍÍÎÑÒÅÉ ÒÅ×ÅÍÈß È ÑÓÌÌÀÐÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÍÎÃÎÑÒÓÏÅÍ×ÀÒÎÃÎ ÎÑÅÂÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ

86–94
(9)

Ðàä÷åíêî Í. È.,
Êàíòîð Ñ. À.

INCREASING THE EFFICIENCY OF GAS TURBINE UNITES BY HEAT RECUPERATION WITH INTAKE AIR COOLING

ϲÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÓÑÒÀÍÎÂÎÊ ÐÅÊÓÏÅÐÀÖ²ªÞ ÒÅÏËÎÒÈ Ç ÎÕÎËÎÄÆÅÍÍßÌ ÏβÒÐß ÍÀ ÂÕÎIJ

ÏÎÂÛØÅÍÈÅ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÓÑÒÀÍÎÂÎÊ ÐÅÊÓÏÅÐÀÖÈÅÉ ÒÅÏËÎÒÛ Ñ ÎÕËÀÆÄÅÍÈÅÌ ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ

95–98
(4)

Ðàä÷åíêî À. Í.,
Ýë Ãåðáè Ðàìçè

RECUPERATIVE GTE INTAKE AIR COOLING BY ABSORPTION AND EJECTOR WASTE HEAT RECOVERY CHILLERS

ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÐÅÊÓÏÅÐÀÒÈÂÍÈÕ ÃÒÄ ÀÁÑÎÐÁÖ²ÉÍÎÞ ÒÀ ÅÆÅÊÒÎÐÍÎÞ ÒÅÏËÎÂÈÊÎÐÈÑÒÎÂÓÞ×ÈÌÈ ÕÎËÎÄÈËÜÍÈÌÈ ÌÀØÈÍÀÌÈ

ÎÕËÀÆÄÅÍÈÅ ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ ÐÅÊÓÏÅÐÀÒÈÂÍÛÕ ÃÒÄ ÀÁÑÎÐÁÖÈÎÍÍÎÉ È ÝÆÅÊÒÎÐÍÎÉ ÒÅÏËÎÈÑÏÎËÜÇÓÞÙÈÌÈ ÕÎËÎÄÈËÜÍÛÌÈ ÌÀØÈÍÀÌÈ

99–103
(5)

Ðàä÷åíêî Ð. Í.

ANALISIS OF ALTERNATIVE VARIANTS FOR COOLING OF CYCLIC AIR OF LOW SPEED DIESEL ENGINE OF TRANSPORT SHIP

ÀÍÀË²Ç ÀËÜÒÅÐÍÀÒÈÂÍÈÕ ÂÀвÀÍҲ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

ÀÍÀËÈÇ ÀËÜÒÅÐÍÀÒÈÂÍÛÕ ÂÀÐÈÀÍÒÎÂ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

104–108
(5)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Ôåäîðîâè÷ O. Å.,
Ëåùåíêî Þ. À.

STRATEGY OF CONTINUOUS IMPROVEMENT QUALITY IN THE LOGISTICS CHAIN OF AEROSPACE PRODUCTION

ÑÒÐÀÒÅÃ²ß ÏÎÑ˲ÄÎÂÍÎÃÎ ÏÎË²ÏØÅÍÍß ßÊÎÑÒ² Ó ËÎòÑÒÈ×ÍÎÌÓ ËÀÍÖÞDz ÂÈÐÎÁÍÈÖÒÂÀ

ÑÒÐÀÒÅÃÈß ÏÎÑËÅÄÎÂÀÒÅËÜÍÎÃÎ ÓËÓרÅÍÈß ÊÀ×ÅÑÒÂÀ  ËÎÃÈÑÒÈ×ÅÑÊÎÉ ÖÅÏÈ ÀÝÐÎÊÎÑÌÈ×ÅÑÊÎÃÎ ÏÐÎÈÇÂÎÄÑÒÂÀ

109–112
(4)

 

 

 

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 áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); CiteFactor; Google Scholar (áèáëèîìåòðè÷åñêèå ïîêàçàòåëè – quot.=1892 / h = 11 / i10 = 25).