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 |
Íàçâàíèå ñòàòüè (article title) |
Ñòðàíèöû (pages) |
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English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
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Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
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Íàðûæíûé À. Ã., |
THE THERMOMECHANICAL MODEL OF CUTTING
PROCESS BY CUTTING TOOLS WITH THE WEAR-RESISTANT COATING |
ÒÅÐÌÎÌÅÕÀͲ×ÍÀ ÌÎÄÅËÜ ÏÐÎÖÅÑÓ Ð²ÇÀÍÍß
вÆÓ×ÈÌ ²ÍÑÒÐÓÌÅÍÒÎÌ Ç² ÇÍÎÑÎÑÒ²ÉÊÈÌ ÏÎÊÐÈÒÒßÌ |
ÒÅÐÌÎÌÅÕÀÍÈ×ÅÑÊÀß
ÌÎÄÅËÜ ÏÐÎÖÅÑÑÀ ÐÅÇÀÍÈß ÐÅÇÖÎÌ Ñ ÈÇÍÎÑÎÑÒÎÉÊÈÌ ÏÎÊÐÛÒÈÅÌ |
4–10 |
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 |
11–24 |
|
Ëÿêóí Ñ. Ô., |
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 |
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Ìåõîíîøèí Þ. Ã., |
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 |
Àâðàìîâ Ê. Â., |
NUMERICAL ANALYSIS OF ROCKETS TANKS
BREAKING LOADS |
×ÈÑÅËÜÍÈÉ ÀÍÀË²Ç ÐÓÉͲÂÍÈÕ ÍÀÂÀÍÒÀÆÅÍÜ
ÎÁÐÅÁÐÅÍÈÕ ÁÀʲ ÐÀÊÅÒÎÍÎѲ¯Â |
×ÈÑËÅÍÍÛÉ ÀÍÀËÈÇ
ÐÀÇÐÓØÀÞÙÈÕ ÍÀÃÐÓÇÎÊ ÎÐÅÁÐÅÍÍÛÕ ÁÀÊÎÂ ÐÀÊÅÒÎÍÎÑÈÒÅËÅÉ |
40–46 |
Íèêîëàåâ À. Ã., |
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 |
47–55 |
|
Àìáðîæåâè÷ À. Â., |
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 |
56–63 |
|
Ôîìè÷åâ Ï. À., |
FINITE ELEMENT
METHOD APLICATION IN THE PRE-CALIBRATION STAGE OF AN AIRPLANE SWEPTWING
DISSECTED SECTIONS |
ÇÀÑÒÎÑÓÂÀÍÍß ÌÅÒÎÄÓ ÑʲÍ×ÅÍÈÕ ÅËÅÌÅÍÒ²Â
ÍÀ ÅÒÀϲ ÏÎÏÅÐÅÄÍÜί ÊÀ˲ÁÐÎÂÊÈ ÏÐÅÏÀÐÎÂÀÍÈÕ ÏÅÐÅвDz ÑÒвËÎÏÎIJÁÍÎÃÎ ÊÐÈËÀ
˲ÒÀÊÀ |
64–69 |
|
Õàëèëîâ Ñ. À., |
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 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êðèâîõàòüêî È. Ñ., |
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 |
79–85 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Áîéêî Ë. Ã., |
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 |
Ðàä÷åíêî Í. È., |
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 |
Ðàä÷åíêî À. Í., |
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 |
99–103 |
|
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 |
104–108 |
|
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè,
ïðîãðàììàìè è ïðîåêòàìè |
||||
Ôåäîðîâè÷ O. Å., |
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 |
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).