Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 2
(109). – 114 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 2 (109). –
114 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND
TECHNOLOGY. – 2014. – ¹ 2 (109). – 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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Êóðèí Ì. À. |
SUPPORT OF ADSORPTION INTERACTION WHEN
CUTTING |
ÇÀÁÅÇÏÅ×ÅÍÍß ÀÄÑÎÐÁÖ²ÉÍί ÂÇÀªÌÎIJ¯ ÏÐÈ
ÌÅÕÀͲ×Í²É ÎÁÐÎÁÖ² вÇÀÍÍßÌ |
ÎÁÅÑÏÅ×ÅÍÈÅ
ÀÄÑÎÐÁÖÈÎÍÍÎÃÎ ÂÇÀÈÌÎÄÅÉÑÒÂÈß
ÏÐÈ ÌÅÕÀÍÈ×ÅÑÊÎÉ ÎÁÐÀÁÎÒÊÅ
ÐÅÇÀÍÈÅÌ |
4–8 |
Ìàëàøåíêî Â. Ë., |
THE RESERCH DEFLASHING PROCESS FROM
THE THERMOPLASTIC WORKPIECE |
ÄÎÑË²ÄÆÅÍÍß ÏÐÎÖÅÑÓ ÂÈÄÀËÅÍÍß ÎÁËÎÞ Ç ÄÅÒÀËÅÉ ²Ç ÒÅÐÌÎÏËÀÑҲ |
ÈÑÑËÅÄÎÂÀÍÈÅ ÏÐÎÖÅÑÑÀ ÓÄÀËÅÍÈß ÎÁËÎß Ñ ÄÅÒÀËÅÉ ÈÇ ÒÅÐÌÎÏËÀÑҲ |
9–15 |
Çåìëÿíàÿ Â. Â., |
SPECIFICITY OF THE MIXTURE HEAD
PARTS TELESCOPED JOINTS ASSEMBLY BEFORE THE SOLDERING |
ÎÑÎÁËÈÂÎÑÒ² ÇÁÈÐÀÍÍß Ï²Ä ÏÀÉÊÓ ÒÅËÅÑÊÎϲ×Í²Õ Ç'ªÄÍÀÍÜ ÄÅÒÀËÅÉ Ç̲ØÓÂÀËÜÍί ÃÎËÎÂÊÈ |
ÎÑÎÁÅÍÍÎÑÒÈ ÑÁÎÐÊÈ ÏÎÄ ÏÀÉÊÓ ÒÅËÅÑÊÎÏÈ×ÅÑÊÈÕ ÑÎÅÄÈÍÅÍÈÉ ÄÅÒÀËÅÉ ÑÌÅÑÈÒÅËÜÍÎÉ
ÃÎËÎÂÊÈ |
16–20 |
Ôðîëîâ Å. À., |
RESEARCH OF INFLUENCE
OF THE OPERATION OF CORRECTION ON EXACTNESS OF FORGINGS |
ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÎÏÅÐÀÖ²¯ ÏÐÀÂÊÈ ÍÀ ÒÎ×ͲÑÒÜ
ÏÎÊÎÂÎÊ |
21–24 |
|
Ôðîëîâ Å. À., |
EFFECTIVE
METHODS OF MAKING
THE DOUBLE-LAYER THIN-WALLED WARES |
ÅÔÅÊÒÈÂͲ ÑÏÎÑÎÁÈ ÂÈÃÎÒÎÂËÅÍÍß
ÄÂÎØÀÐÎÂÈÕ ÒÎÍÊÎÑÒ²ÍÍÈÕ
ÂÈÐÎÁ²Â |
ÝÔÔÅÊÒÈÂÍÛÅ ÑÏÎÑÎÁÛ ÈÇÃÎÒÎÂËÅÍÈß ÄÂÓÕÑËÎÉÍÛÕ ÒÎÍÊÎÑÒÅÍÍÛÕ ÈÇÄÅËÈÉ |
25–28 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
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SOME OPERATIONS GENERALIZATIONS
OF THE VECTOR-TENSOR ANALYSIS |
ÄÅßʲ ÓÇÀÃÀËÜÍÅÍÍß ÎÏÅÐÀÖ²É
ÂÅÊÒÎÐÍÎ-ÒÅÍÇÎÐÍÎÃÎ ÀÍÀ˲ÇÓ |
29–32 |
||
Èâàíîâ Ï. È. |
THE PREPARATORY
PHASE OF FILLING PROCESS OF LARGE-AREA PARACHUTES |
ϲÄÃÎÒÎÂ×ÈÉ ÅÒÀÏ ÏÐÎÖÅÑÓ ÍÀÏÎÂÍÅÍÍß
ÏÀÐÀØÓҲ ÂÅËÈÊÈÕ ÏËÎÙÈÍ |
ÏÎÄÃÎÒÎÂÈÒÅËÜÍÛÉ ÝÒÀÏ ÏÐÎÖÅÑÑÀ ÍÀÏÎËÍÅÍÈß ÏÀÐÀØÞÒÎÂ ÁÎËÜØÈÕ ÏËÎÙÀÄÅÉ |
33–38 |
Òèíÿêîâ Ä. Â. |
THE ADJUSTED METHOD OF THE
DETERMINATION OF THE ANGLES OF
GEOMETRICAL TWIST OF TRAPEZOIDAL WING BASED THE
INDUCED DRAG GROWTH FACTOR |
ÓÒÎ×ÍÅÍÀ ÌÅÒÎÄÈÊÀ ÂÈÇÍÀ×ÅÍÍß ÊÓҲ ÃÅÎÌÅÒÐÈ×ÍÎÃÎ
ÑÊÐÓ×ÅÍÍß ÒÐÀÏÅÖ²ªÏÎIJÁÍÎÃÎ ÊÐÈËÀ ÍÀ ÎÑÍβ ÊÎÅÔ²Ö²ªÍÒÀ
ÇÐÎÑÒÀÍÍß ²ÍÄÓÊÒÈÂÍÎÃÎ ÎÏÎÐÓ |
39–45 |
|
Mukhina M. P. |
ERROR MODEL OF HEADING CHANNEL IN VISION-BASED CORRELATION-EXTREME
NAVIGATION |
ÌÎÄÅËÜ ÏÎÕÈÁÎÊ ÊÀÍÀËÓ ÊÓÐÑÓ Â²ÇÓÀËÜÍί ÊÎÐÅËßÖ²ÉÍÎ-ÅÊÑÒÐÅÌÀËÜÍί
ÍÀ²ÃÀÖ²ÉÍί ÑÈÑÒÅÌÈ |
ÌÎÄÅËÜ ÏÎÃÐÅØÍÎÑÒÅÉ
ÊÀÍÀËÀ ÊÓÐÑÀ ÂÈÇÓÀËÜÍÎÉ ÊÎÐÐÅËßÖÈÎÍÍÎ - ÝÊÑÒÐÅÌÀËÜÍÎÉ ÍÀÂÈÃÀÖÈÎÍÍÎÉ ÑÈÑÒÅÌÛ |
46–52 |
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ |
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Ðûæåíêî À. È., |
SHAPING OF TURBOPROP’S
ANNULAR AIR INTAKES |
ÏÐÎÔ²ËÞÂÀÍÍß Ê²ËÜÖÅÂÈÕ ÏβÒÐÎÇÀÁ²ÐÍÈʲ ÒÓÐÁÎÃÂÈÍÒÎÂÈÕ ÄÂÈÃÓͲ |
ÏÐÎÔÈËÈÐÎÂÀÍÈÅ ÊÎËÜÖÅÂÛÕ ÂÎÇÄÓÕÎÇÀÁÎÐÍÈÊÎÂ ÒÓÐÁÎÂÈÍÒÎÂÛÕ
ÄÂÈÃÀÒÅËÅÉ |
53–58 |
Äàðèÿ çàäå Ñ., |
NUMERICAL METHOD FOR DETERMINATION OF
EFFECTIVE CHARACTERISTICS IN UNIDIRECTIONAL REINFORCED COMPOSITES HEXAGONAL STRUCTURE |
×ÈÑÅËÜÍÀ ÌÅÒÎÄÈÊÀ ÇÍÀÕÎÄÆÅÍÍß ÅÔÅÊÒÈÂÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÎÄÍÎÑÏÐßÌÎÂÀÍÎ ÀÐÌÎÂÀÍÈÕ
ÊÎÌÏÎÇÈҲ ÃÅÊÑÀÃÎÍÀËÜÍβ ÑÒÐÓÊÒÓÐÈ |
59–66 |
|
Ãàâðèëêî Â. Â. |
DESIGNING OF ULTRALIGHT UNMANNED AIRCRAFT USING NEW COMPOSITE
MATERIALS |
ÊÎÍÑÒÐÓÞÂÀÍÍß
ÍÀÄËÅÃÊÈÕ ÁÅÇϲËÎÒÍÈÕ Ë²ÒÀËÜÍÈÕ ÀÏÀÐÀÒ²Â Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÍÎÂÈÕ ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲ |
67–76 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
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Loboda I. I., |
IJÀÃÍÎÑÒÎÂÀͲÑÒÜ ÃÒÄ ÍÀ
Ç̲ÍÍÈÕ ÑÒÀÒÈ×ÍÈÕ ÐÅÆÈÌÀÕ |
ÄÈÀÃÍÎÑÒÈÐÓÅÌÎÑÒÜ ÃÒÄ ÍÀ ÏÅÐÅÌÅÍÍÛÕ ÑÒÀÒÈ×ÅÑÊÈÕ ÐÅÆÈÌÀÕ |
77–85 |
|
Ãóáèí Ñ. Â., |
SIMULATION OF THERMAL
STABILIZATION PROCESS FOR MEASUREMENT OF SOLAR CELL THERMAL CHARACTERISTICS |
ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅÑÓ ÑÒÀÁ²Ë²ÇÀÖ²¯ ÒÅÌÏÅÐÀÒÓÐÈ
ÄËß ÂÈ̲ÐÞÂÀÍÍß ÒÅÏËÎÂÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÔÎÒÎÏÅÐÅÒÂÎÐÞÂÀײ ÇÀÑÒÎÑÓÂÀÍÍß |
86–90 |
|
Ñëþñàðü Ä. Â. |
INTEGRAL CHARACTERISTICS
OF THE DISCHARGE IN THE INVERSE MAGNETRON WITH GAS ANODE, PARTITIONED CATHOD UNITS AND AXIAL PLASMA FLOWS |
ËÎÊÀËÜͲ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÏËÀÇÌÈ Â ²ÍÂÅÐÑÍÎÌÓ
ÌÀÃÍÅÒÐÎͲ Ç ÃÀÇÎÂÈÌ ÀÍÎÄÎÌ, ÑÅÊÖ²ÎÍÎÂÀÍÈÌÈ ÊÀÒÎÄÍÈÌÈ
ÂÓÇËÀÌÈ ² ÎÑÜÎÂÈÌÈ ÏÎÒÎÊÀÌÈ ÏËÀÇÌÈ |
91–95 |
|
Ïîäà Â. Á. |
ESTIMATION OF EFFICIENCY OF APPLICATION IN THE PISTON
ENGINES OF GAS-DISTRIBUTING
MECHANISMS WITH THE REVERSE-ACTING VALVES |
ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ² ÇÀÑÒÎÑÓÂÀÍÍß Â ÏÎÐØÍÅÂÈÕ
ÄÂÈÃÓÍÀÕ ÃÀÇÎÐÎÇÏÎIJËÜÍÈÕ ÌÅÕÀͲÇ̲ ²Ç ÊËÀÏÀÍÀÌÈ ÇÂÎÐÎÒÍί IJ¯ |
96–102 |
|
Ñèðåíêî Ô. Ô., |
SYNTHESIS OF A
DYNAMIC MODEL OF STARTING OF A THREE-SPOOL TFE |
ÑÈÍÒÅÇ ÄÈÍÀ̲×Íί ÌÎÄÅ˲ ÒÐÜÎÕÂÀËÜÍÎÃÎ ÄÂÎÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ÅÒÀϲ ÇÀÏÓÑÊÓ |
ÑÈÍÒÅÇ ÄÈÍÀÌÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÒÐÅÕÂÀËÜÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀ ÝÒÀÏÅ ÇÀÏÓÑÊÀ |
103–108 |
Ãóáèí Ñ. Â., |
FUNCTIONALITY
ANALYSIS OF POWER PROPULSION MODULE FOR SMALL SPACECRAFT |
ÀÍÀË²Ç ÔÓÍÊÖ²ÎÍÀËÜÍÈÕ
ÌÎÆËÈÂÎÑÒÅÉ ÅÍÅÐÃÎÄÂÈÃÓÍÍÎÃÎ ÌÎÄÓËß ÄËß ÌÀËÈÕ
ÊÎÑ̲×ÍÈÕ ÀÏÀÐÀҲ |
ÀÍÀËÈÇ ÔÓÍÊÖÈÎÍÀËÜÍÛÕ ÂÎÇÌÎÆÍÎÑÒÅÉ ÝÍÅÐÃÎÄÂÈÃÀÒÅËÜÍÎÃÎ
ÌÎÄÓËß ÄËß ÌÀËÛÕ ÊÎÑÌÈ×ÅÑÊÈÕ
ÀÏÏÀÐÀÒÎÂ |
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, (http://elibrary.ru); Index Copernicus (Ïîëüøà); Google Scholar.