Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2012. – ¹ 5(92). – 120 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 5(92). – 120
ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 5(92). – 120 p.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Êðàøàíèöà Þ.À. |
N.Ye.
ZHUKOVSKIY - AEROHYDRODYNAMICS AND THE THEORY OF FLIGHT, MATHEMATICS AND MECHANICS: PAST, PRESENT AND
FUTURE |
Ì.ª. ÆÓÊÎÂÑÜÊÈÉ - ÀÅÐÎòÄÐÎÄÈÍÀ̲ÊÀ ² ÒÅÎÐ²ß ÏÎËÜÎÒÓ, ÌÀÒÅÌÀÒÈÊÀ ² ÌÅÕÀͲÊÀ: ÌÈÍÓËÅ, ÑÜÎÃÎÄÅÍÍß É ÌÀÉÁÓÒͪ |
5–10 |
|
Àìáðîæåâè÷ À.Â., |
COMPLEX TRAJECTORY MODEL OF THE AIRCRAFT |
ÊÎÌÏËÅÊÑͲ ÒÐÀªÊÒÎÐͲ ÌÎÄÅ˲ ˲ÒÀËÜÍÈÕ
ÀÏÀÐÀҲ |
11–20 |
|
Ãèðüêà Þ.Â., |
RESEARCHES OF WING AERODYNAMIC
CHARACTERISTICS IN THE ENVIRONMENT DIVISION
PLANE |
ÌÀÒÅÌÀÒÈ×ÍÅ ÌÎÄÅËÞÂÀÍÍß ÂÇÀªÌÎIJ¯ Â’ßÇÊί ÑÒÐÓÌÈÍÈ Ç ÊÐÈÂÎ˲ͲÉÍÎÞ ÏÎÂÅÐÕÍÅÞ |
ÌÀÒÅÌÀÒÈ×ÅÑÊÎÅ
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÂÇÀÈÌÎÄÅÉÑÒÂÈß ÂßÇÊÎÉ ÑÒÐÓÈ Ñ ÍÅÑÓÙÅÉ ÏÎÂÅÐÕÍÎÑÒÜÞ |
21–23 |
Çàéîí÷êîâñêèé Ã.È., |
Throttle cavitation generators and IT’S application in technology |
ÄÐÎÑÅËÜͲ ÊÀ²ÒÀÖ²ÉͲ ÃÅÍÅÐÀÒÎÐÈ ÒÀ ¯Õ
ÇÀÑÒÎÑÓÂÀÍÍß Â ÒÅÕÍÈÖ² |
ÄÐÎÑÑÅËÜÍÛÅ
ÊÀÂÈÒÀÖÈÎÍÍÛÅ ÃÅÍÅÐÀÒÎÐÛ È ÈÕ ÏÐÈÌÅÍÅÍÈÅ Â ÒÅÕÍÈÊÅ |
24–30 |
Ëåáåäü Â.Ã., |
METHOD OF
CALCULATING AERODYNAMIC WIND POWER PLANTS WITH CONCENTRATORS OF AIR FLOW |
ÌÅÒÎÄ ÀÅÐÎÄÈÍÀ̲×ÍÎÃÎ ÐÎÇÐÀÕÓÍÊÓ
²ÒÐÎÅÍÅÐÃÅÒÈ×Íί ÓÑÒÀÍÎÂÊÈ Ç
ÊÎÍÖÅÍÒÐÀÒÎÐÎÌ ÏβÒÐßÍÎÃÎ ÏÎÒÎÊÓ |
ÌÅÒÎÄ
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÐÀÑ×ÅÒÀ ÂÅÒÐÎÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ ÓÑÒÀÍÎÂÊÈ Ñ ÊÎÍÖÅÍÒÐÀÒÎÐÎÌ ÂÎÇÄÓØÍÎÃÎ
ÏÎÒÎÊÀ |
31–42 |
Êðàøàíèöà Þ.À. |
METHOD OF
BOUNDARY INTEGRAL EQUATIONS IN
PLANE VISCOUS FLUID DYNAMICS PROBLEMS |
ÌÅÒÎÄ ÃÐÀÍÈ×ÍÈÕ
²ÍÒÅÃÐÀËÜÍÈÕ Ð²ÂÍßÍÜ Â ÏËÎÑÊÈÕ
ÇÀÄÀ×ÀÕ ÄÈÍÀ̲ÊÈ Â'ßÇÊί вÄÈÍÈ |
ÌÅÒÎÄ ÃÐÀÍÈ×ÍÛÕ
ÈÍÒÅÃÐÀËÜÍÛÕ ÓÐÀÂÍÅÍÈÉ Â ÏËÎÑÊÈÕ ÇÀÄÀ×ÀÕ ÄÈÍÀÌÈÊÈ ÂßÇÊÎÉ ÆÈÄÊÎÑÒÈ |
43–46 |
Òèìîøåíêî Â.È., |
UNSTREADY FLUID
FLOWS IN COMPLEX MANIFOLD SYSTEMS |
ÍÅÑÒÀ˲ ÒÅײ¯ вÄÈÍÈ Ó ÑÊËÀÄÍÈÕ ÐÎÇÃÀËÓÆÅÍÈÕ
ÒÐÓÁÎÏÐβÄÍÈÕ ÑÈÑÒÅÌÀÕ |
ÍÅÓÑÒÀÍÎÂÈÂØÈÅÑß
ÒÅ×ÅÍÈß ÆÈÄÊÎÑÒÈ Â ÑËÎÆÍÛÕ ÐÀÇÂÅÒÂËÅÍÍÛÕ ÒÐÓÁÎÏÐÎÂÎÄÍÛÕ ÑÈÑÒÅÌÀÕ |
47–57 |
Øëàïàöüêèé Â.Î., |
NUMERICAL SIMULATION OF A HELICOPTER DIFFERENT DESIGN TAIL ROTOR
OPERATION |
×ÈÑËÎÂÅ
ÌÎÄÅËÞÂÀÍÍß ÐÎÁÎÒÈ ÂÅÐÒÎ˲ÒÍÎÃÎ ÐÓËÜÎÂÎÃÎ ÃÂÈÍÒÀ вÇÍÈÕ ÔÎÐÌ |
×ÈÑËÅÍÍÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÐÀÁÎÒÛ
ÂÅÐÒÎËÅÒÍÎÃÎ ÐÓËÅÂÎÃÎ ÂÈÍÒÀ ÐÀÇËÈ×ÍÛÕ
ÔÎÐÌ |
58–62 |
Ìîâ÷àí Â.Ò., |
ALGEBRAICALLY-DIFFERENTIAL MODELS OF TURBULENT VISCOSITY COEFFICIENT FOR SHEAR FLOWS |
ÀËÃÅÁÐÎ-ÄÈÔÅÐÅÍÖ²ÀËÜͲ
ÌÎÄÅ˲ ÊÎÅÔ²Ö²ªÍÒÀ ÒÓÐÁÓËÅÍÒÍί Â’ßÇÊÎÑÒ² ÄËß ÏÐÈÑÒ²ÍÍÈÕ ÒÅ×²É |
ÀËÃÅÁÐÎ-ÄÈÔÅÐÅÍÖ²ÀËÜÍÛÅ ÌÎÄÅËÈ ÊÎÝÔÔ²Ö²ÅÍÒÀ
ÒÓÐÁÓËÅÍÒÍÎÉ ÂßÇÊÎÑÒÈ ÄËß ÏÐÈÑÒÅÍÍÛÕ ÒÅ×ÅÍÈÉ |
63–70 |
Ñåëåçîâ È.Ò. |
ON INTERACTION
OF ELASTIC PLATE WITH COMPRESSIBLE GASE STREAM |
ÏÐÎ ÂÇÀªÌÎÄ²Þ ÏÐÓÆÍί ÏËÀÑÒÈÍÈ Ç
ÏÎÒÎÊÎÌ ÃÀÇÓ, ÙÎ ÑÒÈÑÊÀªÒÜÑß |
71–74 |
|
Ïóñòîâîéòîâ Â.Ï. |
Long-Period Motion Stability of Regional Turboprop Aircraft with Pilot Maintaining the Selected Flight
Path Angle |
Ñò³éê³ñòü äîâãîïåð³îäè÷íîãî ðóõó òóðáîãâèíòîâîãî ë³òàêà ïðè âèòðèìóâàíí³ çàäàíîãî êóòà íàõèëó
òðàºêòî𳿠ïîëüîòó |
75–80 |
|
Ñàõíî À. Ã. |
QUALITATIVE ANALYSIS EQUATIONS
OF MOTION OF AIRCRAFT |
ßʲÑÍÈÉ ÀÍÀË²Ç Ð²ÂÍßÍÜ ÐÓÕÓ Ë²ÒÀÒÅËÜÍÎÃÎ
ÀÏÀÐÀÒÓ |
ÊÀ×ÅÑÒÂÅÍÍÛÉ ÀÍÀËÈÇ
ÓÐÀÂÍÅÍÈÉ ÄÂÈÆÅÍÈß ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ |
81–88 |
Åðøîâ Ñ.Â. |
DEVELOPMENT OF APPLICATION PACKAGE FOR 3D FLOW COMPUTATIONS |
ÐÎÇÂÈÒÎÊ ÊÎÌÏËÅÊÑÓ ÏÐÎÃÐÀÌ ÄËß ÐÎÇÐÀÕÓÍÊÓ
ÒÐÈÂÈ̲ÐÍÈÕ ÒÅ×²É Â’ßÇÊÎÃÎ ÃÀÇÓ |
ÐÀÇÂÈÒÈÅ ÊÎÌÏËÅÊÑÀ
ÏÐÎÃÐÀÌÌ ÄËß ÐÀÑ×ÅÒÀ ÒÐÅÕÌÅÐÍÛÕ ÒÅ×ÅÍÈÉ ÂßÇÊÎÃÎ ÃÀÇÀ |
89–94 |
Æåëòîâîäîâ À.À. |
development mechanismS and numerical modelling possibilities of supersonic turbulent separated flows |
ÇÀÊÎÍÎ̲ÐÍÎÑÒ² ÐÎÇÂÈÒÊÓ ÒÀ ÌÎÆËÈÂÎÑÒ² ×ÈÑËÎÂÎÃÎ
ÌÎÄÅËÞÂÀÍÍß ÍÀÄÇÂÓÊÎÂÎÃÎ ÒÓÐÁÓËÅÍÒÍÎÑÒ² ²ÄÐÈÂÍί ÒÅײ¯ |
95–107 |
|
Æóíü Ã.Ã. |
DEVELOPMENT OF
THE ADVANCED HEAT-SHIELDING DESIGN OF KRIOSOSUD |
ÐÎÇÐÎÁÊÀ ÓÄÎÑÊÎÍÀËÅÍί ÒÅÏËÎÇÀÕÈÑÍί
ÊÎÍÑÒÐÓÊÖ²¯ ÊвÎÑÎÑÓÄÓ |
ÐÀÇÐÀÁÎÒÊÀ
ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÍÎÉ ÒÅÏËÎÇÀÙÈÒÍÎÉ ÊÎÍÑÒÐÓÊÖÈÈ ÊÐÈÎÑÎÑÓÄÀ |
108–107 |
Êàøàíîâ À.Ý., |
THE ASSESSMENT
OF TECHNICAL RISKS DURING DNEPR LV LAUNCH |
ÎÖ²ÍÊÀ ÒÅÕͲ×ÍÈÕ ÐÈÇÈÊ²Â Ï²Ä ×ÀÑ ÏÓÑÊÓ
ÐÀÊÅÒÈ-ÍÎÑ²ß «ÄͲÏÐλ |
ÎÖÅÍÊÀ
ÒÅÕÍÈ×ÅÑÊÈÕ ÐÈÑÊΠÏÐÈ ÏÓÑÊÅ ÐÀÊÅÒÛ- ÍÎÑÈÒÅËß «ÄÍÅÏл |
113–118 |
Óâàæàåìûå ÷èòàòåëè!
Íàó÷íî-òåõíè÷åñêèé æóðíàë “ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß
ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß“
âêëþ÷åí â ïåðå÷åíü íàó÷íûõ èçäàíèé, â êîòîðûõ
ìîãóò ïóáëèêîâàòüñÿ îñíîâíûå ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò (ñì.
ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009ã)
Ðåôåðàòèâíàÿ èíôîðìàöèÿ ñîõðàíÿåòñÿ:
– â
îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà íàóêîâà» è ïóáëèêóåòñÿ
â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ ÓÐÆ «Äæåðåëî» (ñâîáîäíûé îí-ëàéíîâûé
äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua),
– 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).