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.

 

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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

Í.Å. ÆÓÊÎÂÑÊÈÉ – ÀÝÐÎÃÈÄÐÎÄÈÍÀÌÈÊÀ È ÄÈÍÀÌÈÊÀ ÏÎËÅÒÀ, ÒÅÎÐÈß È ÏÐÀÊÒÈÊÀ, ÍÀÑËÅÄÈÅ, ÐÀÇÂÈÒÈÅ È ÏÅÐÑÏÅÊÒÈÂÛ

5–10
(6)

Àìáðîæåâè÷ À.Â.,
Áîé÷óê È.Ï.,
Äîëæåíêî È.Þ.,
Ìèãàëèí Ê.Â.,
Ñåðåäà Â.À.

COMPLEX TRAJECTORY MODEL OF THE AIRCRAFT

ÊÎÌÏËÅÊÑͲ ÒÐÀªÊÒÎÐͲ ÌÎÄÅ˲ ˲ÒÀËÜÍÈÕ ÀÏÀÐÀÒ²Â

ÊÎÌÏËÅÊÑÍÛÅ ÒÐÀÅÊÒÎÐÍÛÅ ÌÎÄÅËÈ ËÅÒÀÒÅËÜÍÛÕ ÀÏÏÀÐÀÒÎÂ

11–20
 (10)

Ãèðüêà Þ.Â.,
Êðàøàíèöà Þ.À.

RESEARCHES OF WING AERODYNAMIC CHARACTERISTICS  IN THE ENVIRONMENT DIVISION PLANE

ÌÀÒÅÌÀÒÈ×ÍÅ ÌÎÄÅËÞÂÀÍÍß ÂÇÀªÌÎIJ¯ ÂßÇÊί ÑÒÐÓÌÈÍÈ  Ç ÊÐÈÂÎ˲ͲÉÍÎÞ ÏÎÂÅÐÕÍÅÞ

ÌÀÒÅÌÀÒÈ×ÅÑÊÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÂÇÀÈÌÎÄÅÉÑÒÂÈß ÂßÇÊÎÉ ÑÒÐÓÈ Ñ ÍÅÑÓÙÅÉ ÏÎÂÅÐÕÍÎÑÒÜÞ

21–23
 (3)

Çàéîí÷êîâñêèé Ã.È.,
Òàðàñåíêî Ò.Â.,
Ëàíåöêèé Â.Ã.,
Ïóçèê À.Ñ.

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
 (7)

Ëåáåäü Â.Ã.,
Êàëêàìàíîâ Ñ.À.

METHOD OF CALCULATING AERODYNAMIC WIND POWER PLANTS  WITH CONCENTRATORS OF AIR FLOW

ÌÅÒÎÄ ÀÅÐÎÄÈÍÀ̲×ÍÎÃÎ ÐÎÇÐÀÕÓÍÊÓ Â²ÒÐÎÅÍÅÐÃÅÒÈ×Íί ÓÑÒÀÍÎÂÊÈ  Ç ÊÎÍÖÅÍÒÐÀÒÎÐÎÌ ÏβÒÐßÍÎÃÎ ÏÎÒÎÊÓ

ÌÅÒÎÄ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÐÀÑ×ÅÒÀ ÂÅÒÐÎÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ ÓÑÒÀÍÎÂÊÈ Ñ ÊÎÍÖÅÍÒÐÀÒÎÐÎÌ ÂÎÇÄÓØÍÎÃÎ ÏÎÒÎÊÀ

31–42
 (12)

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
 (4)

Òèìîøåíêî Â.È.,
Êíûøåíêî Þ.Â.

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
(11)

Øëàïàöüêèé Â.Î.,
Ìèðãîðîä Þ.².,
Áåðäî÷íèê Â.À.

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
(5)

Ìîâ÷àí Â.Ò.,
Øêâàð ª.Î.,
Êîçëîâà Ò.Â.

ALGEBRAICALLY-DIFFERENTIAL MODELS OF TURBULENT  VISCOSITY COEFFICIENT FOR SHEAR FLOWS

ÀËÃÅÁÐÎ-ÄÈÔÅÐÅÍÖ²ÀËÜͲ ÌÎÄÅ˲ ÊÎÅÔ²Ö²ªÍÒÀ ÒÓÐÁÓËÅÍÒÍί Â’ßÇÊÎÑÒ² ÄËß ÏÐÈÑÒ²ÍÍÈÕ ÒÅײÉ

ÀËÃÅÁÐÎ-ÄÈÔÅÐÅÍÖ²ÀËÜÍÛÅ ÌÎÄÅËÈ ÊÎÝÔÔ²Ö²ÅÍÒÀ ÒÓÐÁÓËÅÍÒÍÎÉ  ÂßÇÊÎÑÒÈ  ÄËß ÏÐÈÑÒÅÍÍÛÕ ÒÅ×ÅÍÈÉ

63–70
(8)

Ñåëåçîâ È.Ò.

ON INTERACTION OF ELASTIC PLATE WITH COMPRESSIBLE GASE STREAM

ÏÐÎ ÂÇÀªÌÎÄ²Þ ÏÐÓÆÍί ÏËÀÑÒÈÍÈ Ç ÏÎÒÎÊÎÌ ÃÀÇÓ, ÙÎ ÑÒÈÑÊÀªÒÜÑß

Î ÂÇÀÈÌÎÄÅÉÑÒÂÈÈ ÓÏÐÓÃÎÉ ÏËÀÑÒÈÍÛ Ñ ÏÎÒÎÊÎÌ ÑÆÈÌÀÅÌÎÃÎ ÃÀÇÀ

71–74
 (4)

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

ÓÑÒÎÉ×ÈÂÎÑÒÜ ÄËÈÍÍÎÏÅÐÈÎÄÈ×ÅÑÊÎÃÎ ÄÂÈÆÅÍÈß ÒÓÐÁÎÂÈÍÒÎÂÎÃÎ ÐÅÃÈÎÍÀËÜÍÎÃÎ ÑÀÌÎËÅÒÀ ÏÐÈ ÂÛÄÅÐÆÈÂÀÍÈÈ ËÅÒ×ÈÊÎÌ ÇÀÄÀÍÍÎÃÎ ÓÃËÀ ÍÀÊËÎÍÀ ÒÐÀÅÊÒÎÐÈÈ ÏÎËÅÒÀ

75–80
(6)

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
(8)

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
 (6)

Æåëòîâîäîâ À.À.

development mechanismS and numerical modelling possibilities  of supersonic turbulent separated flows

ÇÀÊÎÍÎ̲ÐÍÎÑÒ² ÐÎÇÂÈÒÊÓ ÒÀ ÌÎÆËÈÂÎÑÒ² ×ÈÑËÎÂÎÃÎ ÌÎÄÅËÞÂÀÍÍß ÍÀÄÇÂÓÊÎÂÎÃÎ ÒÓÐÁÓËÅÍÒÍÎÑÒ² ²ÄÐÈÂÍί ÒÅײ¯

ÇÀÊÎÍÎÌÅÐÍÎÑÒÈ ÐÀÇÂÈÒÈß È ÂÎÇÌÎÆÍÎÑÒÈ ×ÈÑËÅÍÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÑÂÅÐÕÇÂÓÊÎÂÛÕ ÒÓÐÁÓËÅÍÒÍÛÕ ÎÒÐÛÂÍÛÕ ÒÅ×ÅÍÈÉ

95–107
(13)

Æóíü Ã.Ã.

DEVELOPMENT OF THE ADVANCED HEAT-SHIELDING DESIGN OF KRIOSOSUD

ÐÎÇÐÎÁÊÀ ÓÄÎÑÊÎÍÀËÅÍί ÒÅÏËÎÇÀÕÈÑÍί ÊÎÍÑÒÐÓÊÖ²¯ ÊвÎÑÎÑÓÄÓ

ÐÀÇÐÀÁÎÒÊÀ ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÍÎÉ ÒÅÏËÎÇÀÙÈÒÍÎÉ ÊÎÍÑÒÐÓÊÖÈÈ ÊÐÈÎÑÎÑÓÄÀ

108–107
(5)

Êàøàíîâ À.Ý.,
Äåãòÿðåâ À.Â.,
Ãëàäêèé Ý.Ã.,
Áàðàíîâ Å.Þ.

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
 (6)

 

 

 

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).