Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 4
(111). – 107 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 4 (111). –
107 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2014. – ¹ 4 (111). – 107 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 |
||||
Çàéöåâ Â. Å., |
INVESTIGATION OF THE CUT MAIN
PARAMETERS INFLUENCE TO SURFACE ROUGHNESS
Ra OF ALUMINUM ALLOY 6082 T6 MILLING |
ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÎÑÍÎÂÍÈÕ ÏÀÐÀÌÅÒвÂ
вÇÀÍÍß ÍÀ ÂÅËÈ×ÈÍÓ ØÎÐÑÒÊÎÑÒ² ÏÎÂÅÐÕͲ Ra ÏÐÈ
ÒÎÐÖÅÂÎÌÓ ÔÐÅÇÅÐÓÂÀÍͲ ÀËÞ̲ͲªÂÈÕ ÑÏËÀ² 6082 Ò6 |
ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÎÑÍÎÂÍÛÕ
ÏÀÐÀÌÅÒÐΠÐÅÇÀÍÈß ÍÀ ÂÅËÈ×ÈÍÓ ØÅÐÎÕÎÂÀÒÎÑÒÈ ÏÎÂÅÐÕÍÎÑÒÈ Ra
ÏÐÈ ÒÎÐÖÅÂÎÌ ÔÐÅÇÅÐÎÂÀÍÈÈ ÀËÞÌÈÍÈÅÂÎÃÎ ÑÏËÀÂÀ 6082 Ò6 |
4–9 |
Êîøåâîé
Í. Ä., |
STUDY AND OPTIMIZATION
OF THE HEAT TREATMENT PROCESS OF THE DETAILS MADE OF
HIGH CARBON STEEL |
ÄÎÑË²ÄÆÅÍÍß
ÒÀ ÎÏÒÈ̲ÇÀÖ²ß ÒÅÕÍÎËÎò×ÍÎÃÎ ÏÐÎÖÅÑÓ ÒÅÐÌÎÎÁÐÎÁÊÈ äåòàëåé Ç âèñîêîâóãëåöåâÈÕ ñòàëÅÉ |
10–13 |
|
Ñèêóëüñêèé
Â. Ò., |
INVESTIGATION OF shaping of double curved stiffened panels with complex
inner geometry |
äîñë³äæåííÿ
ïðîöåñó ôîðìîóòâîðåííÿ îðåáðåíèõ ïàíåëåé ïîäâ³éíî¿ êðèâèçíè ç³ ñêëàäíîþ
âíóòð³øíüîþ ãðàâþðîþ |
14–21 |
|
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Äüÿ÷åíêî À. Þ., |
ANALYSIS METHODS of aerodynamic calculations of
Helicopter’s rotor |
ÀÍÀË²Ç ÌÅÒÎIJÂ
àåðîäèíàì³÷íîãî ðîçðàõóíêó Íåñó÷îãî ãâèíòà ÂÅÐÒÎËÜÎÒÀ |
ÀÍÀËÈÇ ÌÅÒÎÄÎÂ
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÐÀÑ×ÅÒÀ ÍÅÑÓÙÅÃÎ ÂÈÍÒÀ ÂÅÐÒÎËÅÒÀ |
22–33 |
Ìåõîíîøèí
Þ. Ã., |
THE BASIS OF
THE NECESSITY OF THE DEEVELOPMENT, THE CHOICE OF THE CONCEPTION AND PROBLEMATIC ISSUES OF
THE DESIGNING OF AEROSPACE PARACHUTE
SYSTEM |
ÎÁ¥ÐÓÍÒÓÂÀÍÍß ÍÅÎÁÕ²ÄÍÎÑÒ² ÐÎÇÐÎÁÊÈ,
ÂÈÁ²Ð ÊÎÍÖÅÏÖ²¯ ² ÏÐÎÁËÅÌͲ ÏÈÒÀÍÍß
ÏÐÎÅÊÒÓÂÀÍÍß ÏβÒÐßÍÎ-ÊÎÑ̲×Íί ÏÀÐÀØÓÒÍί
ÑÈÑÒÅÌÈ |
34–41 |
|
Ëåáåäü
Â. Ã., |
NONLINEAR MATHEMATICAL MODEL OF rotor aerodynamics for modeling flight dynamics ON helicopter
simulators |
ÌÀÒÅÌÀÒÈ×ÍÀ
ÌÎÄÅËÜ ÍÅ˲ͲÉÍί àåðîäèíàì³êè íåñó÷îãî ãâèíòà ÄËß ÇÀÄÀ× ÌÎÄÅËÞÂÀÍÍß ÄÈÍÀ̲ÊÈ ÏÎËÜÎÒÓ ÍÀ âåðòîëÜÎòíèõ òðåíàæåðàõ |
42–48 |
|
Íèêîëàåâ
À. Ã., |
ELASTIC SPACE WITH FOUR SPHEROIDAL INCLUSIONS UNDER EXTERNAL LOAD |
ÏÐÓÆÍÈÉ
ÏÐÎÑÒ²Ð Ç ×ÎÒÈÐÌÀ ÑÔÅÐίÄÀËÜÍÈÌÈ ÂÊËÞ×ÅÍÍßÌÈ Ï²Ä Ä²ªÞ ÇÎÂͲØÍ²Õ ÍÀÂÀÍÒÀÆÅÍÜ |
ÓÏÐÓÃÎÅ
ÏÐÎÑÒÐÀÍÑÒÂÎ Ñ ×ÅÒÛÐÜÌß ÑÔÅÐÎÈÄÀËÜÍÛÌÈ ÂÊËÞ×ÅÍÈßÌÈ ÏÎÄ ÄÅÉÑÒÂÈÅÌ ÂÍÅØÍÅÉ
ÍÀÃÐÓÇÊÈ |
49–55 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ðàä÷åíêî À. Í., |
EVALUATION OF COOLING POTENTIAL OF GAS TURBINE UNIT INTAKE AIR BY
TRANSFORMING THE EXHAUST GAS HEAT IN WASTE HEAT RECOVERY COOLING MACHINES |
ÎÖ²ÍÊÀ ÏÎÒÅÍÖ²ÀËÓ ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÓÑÒÀÍÎÂÎÊ ÒÐÀÍÑÔÎÐÌÀÖ²ªÞ
ÒÅÏËÎÒÈ Â²ÄÏÐÀÖÜÎÂÀÍÈÕ ÃÀDz  ÒÅÏËÎÂÈÊÎÐÈÑÒÎÂÓÞ×ÈÕ
ÕÎËÎÄÈËÜÍÈÕ ÌÀØÈÍÀÕ |
56–59 |
|
Ñàôîíîâ
Â. À., |
THERMOMECHANICAL ENGINE WITH LINEAR GENERATOR WORKING
FOR CYCLE STIRLING |
ÒÅÐÌÎÌÅÕÀͲ×ÍÈÉ ÄÂÈÃÓÍ Ç
˲ͲÉÍÈÌ ÃÅÍÅÐÀÒÎÐÎÌ, ÏÐÀÖÞÞ×ÈÉ ÇÀ
ÖÈÊËÎÌ ÑÒ²Ð˲ÍÃÀ |
ÒÅÐÌÎÌÅÕÀÍÈ×ÅÑÊÈÉ
ÄÂÈÃÀÒÅËÜ Ñ ËÈÍÅÉÍÛÌ ÃÅÍÅÐÀÒÎÐÎÌ, ÐÀÁÎÒÀÞÙÈÉ ÏÎ ÖÈÊËÓ ÑÒÈÐËÈÍÃÀ |
60–63 |
Áàðûøåâà
Å. Ñ., |
AIRCRAFT ENGINE AXIS-CENTRIFUGAL COMPRESSOR FLOW INVESTIGATION |
ÄÎÑË²ÄÆÅÍͲ ÒÅײ¯
 ²ÑÜβÄÖÅÍÒÐÎÂÎÌÓ ÊÎÌÏÐÅÑÎв À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÒÅ×ÅÍÈß Â ÎÑÅÖÅÍÒÐÎÁÅÆÍÎÌ ÊÎÌÏÐÅÑÑÎÐÅ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß |
64–69 |
Ê 55 ëåòèþ êàôåäðû
ÑÓËÀ |
||||
Êóëèê À. Ñ., |
AREAS OF
RESEARCH AND INVENTIVE ACTIVITIES OF
AIRCRAFT CONTROL SYSTEMS DEPARTMENT |
ÍÀÏÐßÌÊÈ ÍÀÓÊÎÂÎ-ÄÎÑ˲ÄÍÈÖÜÊÈÕ ÒÀ
ÂÈÍÀÕ²ÄÍÈÖÜÊÈÕ ÐÎÁ²Ò ÍÀ ÊÀÔÅÄв ÑÈÑÒÅÌ
ÓÏÐÀÂ˲ÍÍß Ë²ÒÀËÜÍÈÌÈ ÀÏÀÐÀÒÀÌÈ |
70–75 |
|
Êóëèê À. Ñ., |
PRINCIPLES OF THE USE OF THE LABORATORY DEPARTMENT FUND MANAGEMENT
SYSTEMS AIRCRAFT IN EDUCATIONAL PROCESS AND RESEARCH |
ÏÐÈÍÖÈÏÈ
ÂÈÊÎÐÈÑÒÀÍÍß ËÀÁÎÐÀÒÎÐÍÎÃÎ ÔÎÍÄÓ ÊÀÔÅÄÐÈ ÑÈÑÒÅÌ ÓÏÐÀÂ˲ÍÍß Ë²ÒÀËÜÍÈÌÈ
ÀÏÀÐÀÒÀÌÈ Ó ÍÀÂ×ÀËÜÍÎÌÓ ÏÐÎÖÅѲ ÒÀ ÍÀÓÊÎÂÈÕ ÄÎÑË²ÄÆÅÍÍßÕ |
76–83 |
|
Äæóëãàêîâ
Â. Ã., |
SMALL
AUTONOMOUS UNMANNED SYSTEMS DEPARTMENT OF AIRCRAFT CONTROL |
ÌÀËÎÃÀÁÀÐÈÒͲ
ÀÂÒÎÍÎÌͲ ÁÅÇϲËÎÒͲ ÊÎÌÏËÅÊÑÈ ÊÀÔÅÄÐÈ ÑÈÑÒÅÌ ÓÏÐÀÂ˲ÍÍß Ë²ÒÀËÜÍÈÌÈ ÀÏÀÐÀÒÀÌÈ |
ÌÀËÎÃÀÁÀÐÈÒÍÛÅ
ÀÂÒÎÍÎÌÍÛÅ ÁÅÑÏÈËÎÒÍÛÅ ÊÎÌÏËÅÊÑÛ ÊÀÔÅÄÐÛ ÑÈÑÒÅÌ ÓÏÐÀÂËÅÍÈß ËÅÒÀÒÅËÜÍÛÌÈ
ÀÏÏÀÐÀÒÀÌÈ |
84–96 |
Êóëèê À. Ñ., |
DEVELOPMENT OF
THE COMPUTER-BASED TUTOR PROGRAMS ON
THE AIRCRAFT CONTROL SYSTEMS DEPARTMENT |
ÐÎÇÐÎÁÊÀ ÊÎÌÏ’ÞÒÅÐÍÈÕ ÍÀÂ×ÀÞ×ÈÕ ÏÐÎÃÐÀÌ
ÍÀ ÊÀÔÅÄв ÑÈÑÒÅÌ ÓÏÐÀÂ˲ÍÍß Ë²ÒÀËÜÍÈÌÈ
ÀÏÀÐÀÒÀÌÈ |
ÐÀÇÐÀÁÎÒÊÀ
ÊÎÌÏÜÞÒÅÐÍÛÕ ÎÁÓ×ÀÞÙÈÕ ÏÐÎÃÐÀÌÌ ÍÀ ÊÀÔÅÄÐÅ ÑÈÑÒÅÌ ÓÏÐÀÂËÅÍÈß ËÅÒÀÒÅËÜÍÛÌÈ
ÀÏÏÀÐÀÒÀÌÈ |
97–105 |
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
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- âêëþ÷åí â ìåæäóíàðîäíûå áèáëèîìåòðè÷åñêèå
è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.