Íàöèîíàëüíûé àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé èíñòèòóò”

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2012. – ¹ 9(96). – 274 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 9(96). – 274 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 9(96). – 274 p.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Êàëèíèíà Í.Å.,
Êàâàö Î.À.,
Êàëèíèí Â.Ò.

TECHNOLOGICAL PROPERTIES OF MODIFIED CASTINGS SILUMINS

ÒÅÕÍÎËÎò×Ͳ ÂËÀÑÒÈÂÎÑÒ² ÌÎÄÈÔ²ÊÎÂÀÍÈÕ ËÈÂÀÐÍÈÕ ÑÈËÓ̲ͲÂ

ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÅ ÑÂÎÉÑÒÂÀ ÌÎÄÈÔÈÖÈÐÎÂÀÍÍÛÕ ËÈÒÅÉÍÛÕ ÑÈËÓÌÈÍÎÂ

7–10
(4)

Êðèâöîâ Â.Ñ.,
Êîìáàðîâ Â.Â.,
Ñîðîêèí Â.Ô.

PROBLEMS OF SPLINE INTERPOLATION WITH SMOOTHLY-LIMITED  KINEMATICAL PARAMETERS OF MOVEMENT IN TASKS OF CNC  HIGH-SPEED  EQUIPMENT

ÏÐÎÁËÅÌÈ ÑÏËÀÉÍÎÂî¿ ²ÍÒÅÐÏÎËßÖ²¯ ²Ç ÃËÀÄÊÎ-ÎÁÌÅÆÅÍÈÌÈ Ê²ÍÅÌÀÒÈ×ÍÈÌÈ ÏÀÐÀÌÅÒÐÀÌÈ ÐÓÕÓ â ÇÀÄÀ×ÀÕ ×ÈÑËÎÂÎÃÎ ÏÐÎÃÐÀÌÍÎÃÎ ÊÅÐÓÂÀÍÍß ÂÈÑÎÊÎØÂÈÄʲÑÍÈÌ ÓÑÒÀÒÊÓÂÀÍÍßÌ

ÏÐÎÁËÅÌÛ ÑÏËÀÉÍÎÂÎÉ ÈÍÒÅÐÏÎËßÖÈÈ Ñ ÃËÀÄÊÎÎÃÐÀÍÈ×ÅÍÍÛÌÈ ÊÈÍÅÌÀÒÈ×ÅÑÊÈÌÈ ÏÀÐÀÌÅÒÐÀÌÈ ÄÂÈÆÅÍÈß Â ÇÀÄÀ×ÀÕ ×ÈÑËÎÂÎÃÎ ÏÐÎÃÐÀÌÌÍÎÃÎ ÓÏÐÀÂËÅÍÈß ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÛÌ ÎÁÎÐÓÄÎÂÀÍÈÅÌ

11–19
(9)

Òðåòüÿê Â.Â.

COMPUTATION OF PARAMETERS OF MAGNETIC-IMPULSIVE STAMPING IN OBJECTIVE PRESENTATION

ÐÎÇÐÀÕÓÍÎÊ ÏÀÐÀÌÅÒв ÌÀÃͲÒÍÎ-²ÌÏÓËÜÑÍÎÃÎ ØÒÀÌÏÓÂÀÍÍß Â ÎÁ'ªÊÒÍÎÌÓ ÓßÂËÅÍͲ

ÐÀÑ×ÅÒ ÏÀÐÀÌÅÒÐΠÌÀÃÍÈÒÍÎ-ÈÌÏÓËÜÑÍÎÉ ØÒÀÌÏÎÂÊÈ Â ÎÁÚÅÊÒÍÎÌ ÏÐÅÄÑÒÀÂËÅÍÈÈ

20–24
(5)

Äðàãîáåöêèé Â.Â.,
Õàðëàìîâà Å.Â.,
Øìàíäèé Â.Ì.

DM OF ECOLOGICAL SAFETY DURING REALIZATION OF TECHNOLOGIES OF COLD SPRAYING OF DETAILS OF TURBO-ENGINES OF ËÅÒÅËÜÍÛÕ VEHICLES

ÇÀÁÅÇÏÅ×ÅÍÍß ÅÊÎËÎò×Íί ÁÅÇÏÅÊÈ ÏÐÈ ÐÅÀ˲ÇÀÖ²¯ ÒÅÕÍÎËÎÃ²É ÕÎËÎÄÍÎÃÎ ÍÀÏÈËÅÍÍß ÄÅÒÀËÅÉ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ˲ÒÀËÜÍÈÕ ÀÏÀÐÀÒ²Â

ÎÁÅÑÏÅ×ÅÍÈÅ ÝÊÎËÎÃÈ×ÅÑÊÎÉ ÁÅÇÎÏÀÑÍÎÑÒÈ ÏÐÈ ÐÅÀËÈÇÀÖÈÈ ÒÅÕÍÎËÎÃÈÉ ÕÎËÎÄÍÎÃÎ ÍÀÏÛËÅÍÈß ÄÅÒÀËÅÉ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ËÅÒÀÒÅËÜÍÛÕ ÀÏÏÀÐÀÒÎÂ

25–28
(4)

Êîâàëü÷óê È.À.,
Òðåòüÿê Â.Â.,
Ìàíàíêîâ Î.Â.

PROSPECTS OF THE USE SPRUTEXPRO FOR  DEVELOPMENT  OF CONSTRUCTION AND TECHNOLOGY OF MAKING PURVEYANCES BY IMPULSIVE TECHNOLOGIES

ÏÅÐÑÏÅÊÒÈÂÈ ÂÈÊÎÐÈÑÒÎÂÓÂÀÍÍß SPRUTEXPRO ÄËß ÐÎÇÐÎÁÊÈ  ÊÎÍÑÒÐÓÊÖ²¯ ² ÒÅÕÍÎËÎò¯ ÂÈÃÎÒÎÂËÅÍÍß ÏÎÊÎÂÎÊ  ÇÀ ÄÎÏÎÌÎÃÎÞ ²ÌÏÓËÜÑÍÈÕ ÒÅÕÍÎËÎòÉ

ÏÅÐÑÏÅÊÒÈÂÛ ÈÑÏÎËÜÇÎÂÀÍÈß SPRUTEXPRO ÄËß ÐÀÇÐÀÁÎÒÊÈ ÊÎÍÑÒÐÓÊÖÈÈ È ÒÅÕÍÎËÎÃÈÈ ÈÇÃÎÒÎÂËÅÍÈß ÏÎÊÎÂÎÊ Ñ ÏÎÌÎÙÜÞ ÈÌÏÓËÜÑÍÛÕ ÒÅÕÍÎËÎÃÈÉ

29–33
(5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ëîãèíîâ Â.Â.,
Êðàâ÷åíêî È.Ô.,
Åëàíñêèé À.Â.

Analyses of aerodynamic parameters of regional passenger airplane with different TFE in the system of power plant

äîñë³äæåííÿ àåðîäèíàì³÷íèõ õàðàêòåðèñòèê ðåã³îíàëüíîãî òðàíñïîðòíîãî ë³òàêà ç ð³çíèìè ÒÐÄÄ â ñèñòåì³ ñèëîâî¿ óñòàíîâêè

ÈÑÑËÅÄÎÂÀÍÈÅ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÐÅÃÈÎÍÀËÜÍÎÃÎ ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÀÌÎËÅÒÀ Ñ ÐÀÇËÈ×ÍÛÌÈ ÒÐÄÄ Â ÑÈÑÒÅÌÅ ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÈ

34–39
(6)

Òàðàñîâ À.È.,
Ùèïàêîâ Â.À.

PROBLEMS OF CREATION PULSE DETONATION GAS TURBINE ENGINES

ÏÐÎÁËÅÌÈ ÑÒÂÎÐÅÍÍß ÃÀÇÎÒÓÐÁIÍÍÎÃÎ ÏÓËÜÑÓÞ×ÅÃÎ ÄÅÒÎÍÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ

ÏÐÎÁËÅÌÛ ÑÎÇÄÀÍÈß ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÏÓËÜÑÈÐÓÞÙÅÃÎ ÄÅÒÎÍÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß

40–44
(5)

Êðàéíþê À.È.

PRE-CONDITIONS OF CREATION OF DISK ENGINE REACTIVE ROTATIONS OF CASCADE EXCHANGE PRESSURE

ÏÅÐÅÄÓÌÎÂÈ ÑÒÂÎÐÅÍÍß ÄÈÑÊÎÂÎÃÎ ÄÂÈÃÓÍÀ ÐÅÀÊÒÈÂÍÎÃÎ ÎÁÅÐÒÀÍÍß ÊÀÑÊÀÄÍÎÃÎ ÎÁ̲ÍÓ ÒÈÑÊÎÌ

ÏÐÅÄÏÎÑÛËÊÈ ÑÎÇÄÀÍÈß ÄÈÑÊÎÂÎÃÎ ÄÂÈÃÀÒÅËß ÐÅÀÊÒÈÂÍÎÃÎ ÂÐÀÙÅÍÈß ÊÀÑÊÀÄÍÎÃÎ ÎÁÌÅÍÀ ÄÀÂËÅÍÈÅÌ

45–48
(4)

Øåðåìåòüåâ À.Â.

CONSTRUCTIVE SIMULARITY OF THE AVIATION GTE PARTS

ÊÎÍÑÒÐÓÊÒÈÂÍÀ ÏÎIJÁͲÑÒÜ Ó ÄÅÒÀËßÕ À²ÀÖ²ÉÍÈÕ ÃÒÄ

ÊÎÍÑÒÐÓÊÒÈÂÍÎÅ ÏÎÄÎÁÈÅ Â ÄÅÒÀËßÕ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

49–53
(5)

Òèíÿêîâ Ä.Â.,
Óòåíêîâà Â.Â.

AnalysIs oN Tapered wing shapes of partial criteria of their effectiveness

ÀÍÀË²Ç ÃÅÎÌÅÒÐÈ×ÍÈÕ ÔÎÐÌ ÒÐÀÏÅÖ²ªÏÎIJÁÍÈÕ ÊÐÈË  ÇÀ ×ÀÑÒÈÍÍÈÌÈ ÊÐÈÒÅвßÌÈ ¯Õ ÅÔÅÊÒÈÂÍÎÑÒ²

ÀÍÀËÈÇ ÔÎÐÌ ÒÐÀÏÅÖÈÅÂÈÄÍÛÕ ÊÐÛËÜÅ ÏÎ ×ÀÑÒÍÛÌ ÊÐÈÒÅÐÈßÌ ÈÕ ÝÔÔÅÊÒÈÂÍÎÑÒÈ

54–60
(7)

Ñòåïàíåíêî Ñ.Ì.,
Òåâñ À.À.

ROLE OF OUTSOURCING IN THE SYSTEM OF PROCESSES FOR CREATING NEW AERO ENGINE SPECIMENS

ÐÎËÜ ÀÓÒÑÎÐÑÈÍÃÓ Â ÑÈÑÒÅ̲ ÏÐÎÖÅѲ ÑÒÂÎÐÅÍÍß ÍÎÂÈÕ ÇÐÀÇʲ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÐÎËÜ ÀÓÒÑÎÐÑÈÍÃÀ Â ÑÈÑÒÅÌÅ ÏÐÎÖÅÑÑÎÂ ÑÎÇÄÀÍÈß ÍÎÂÛÕ ÎÁÐÀÇÖÎÂ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

61–65
(5)

Áóãàåíêî Î.Ì.

SIMULATION OF JOINT WORK PROGRAM AND THREE-PHASE ACCELERATION GTE NOZZLE

ÏÐÎÃÐÀÌÀ ÌÎÄÅËÞÂÀÍÍß ÑÓ̲ÑÍί ÐÎÁÎÒÈ ÃÒÄ ÒÀ ÒÐÈÔÀÇÎÂÎÃÎ ÐÎÇòÍÍÎÃÎ ÑÎÏËÀ

ÏÐÎÃÐÀÌÌÀ ÌÎÄÅËÈÐÎÂÀÍÈß ÑÎÂÌÅÑÒÍÎÉ ÐÀÁÎÒÛ ÃÒÄ È ÒÐÅÕÔÀÇÍÎÃÎ ÐÀÇÃÎÍÍÎÃÎ ÑÎÏËÀ

66–70
(5)

Ãðèçóí Ì.Í.,
Åðøîâ Ñ.Â.

CALCULATION OF TWO-DIMENSIONAL INVISCID FLOWS WITH NEWTON METHOD

ÐÎÇÐÀÕÓÍÎÊ ÄÂÎÂÈ̲ÐÍÈÕ ÍÅÂ’ßÇÊÈÕ ÒÅײɠ ÇÀ ÄÎÏÎÌÎÃÎÞ ÌÅÒÎÄÀ ÍÜÞÒÎÍÀ

ÐÀÑ×ÅÒ ÄÂÓÌÅÐÍÛÕ ÍÅÂßÇÊÈÕ ÒÅ×ÅÍÈÉ Ñ ÏÎÌÎÙÜÞ ÌÅÒÎÄÀ ÍÜÞÒÎÍÀ

71–75
(5)

Ñûñîåâ Þ.À.

FEATURES OF CREATION OF SYSTEMS FOR HIGH-PRECISION GAS MIXING

ÎÑÎÁËÈÂÎÑÒ² ÑÒÂÎÐÅÍÍß ÃÀÇÎÇ̲ØÓÞ×ÈÕ ÑÈÑÒÅÌ  ϲÄÂÈÙÅÍί ÒÎ×ÍÎÑÒ²

ÎÑÎÁÅÍÍÎÑÒÈ ÑÎÇÄÀÍÈß ÃÀÇÎÑÌÅØÈÂÀÞÙÈÕ ÑÈÑÒÅÌ ÏÎÂÛØÅÍÍÎÉ ÒÎ×ÍÎÑÒÈ

76–80
(4)

Äîëìàòîâ Ä.À.

SINGLE HYDROCARBON DROP COMBUSTION IN THE PRESENCE OF STATIONARY ARC

ÃÎвÍÍß ÎÄÈÍÎÊί ÊÐÀÏ˲ ÂÓÃËÅÂÎÄÍÅÂÎÃÎ ÏÀËÈÂÀ  Ó ÏÐÈÑÓÒÍÎÑÒ² ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÐÎÇÐßÄÓ

ÃÎÐÅÍÈÅ ÎÄÈÍÎ×ÍÎÉ ÊÀÏËÈ ÓÃËÅÂÎÄÎÐÎÄÍÎÃÎ ÒÎÏËÈÂÀ  ÏÐÈÑÓÒÑÒÂÈÈ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÐÀÇÐßÄÀ

81–86
(6)

Ñîòíèêîâ Â.Ï.

MULTIPROCESSOR APPROXIMATION OF GAS ISOTHERMIC COMPRESSION

ÌÓËÜÒÈÏÐÎÖÅÑÍÀ ÀÏÐÎÊÑÈÌÀÖ²ß ²ÇÎÒÅÐ̲×ÍÎÃÎ ÑÒÈÑÊÀÍÍß ÃÀÇÓ

ÌÓËÜÒÈÏÐÎÖÅÑÑÍÀß ÀÏÏÐÎÊÑÈÌÀÖÈß ÈÇÎÒÅÐÌÈ×ÅÑÊÎÃÎ ÑÆÀÒÈß ÃÀÇÀ

87–92
(6)

Ãàéäà÷óê À.Â.,
×åñíîêîâ À.Â.

CONCEPTION OF OPTIMIZATION OF APPLICATION OF COMPOSITION MATERIALS TAKING INTO ACCOUNT ECONOMIC EFFICIENCY

ÊÎÍÖÅÏÖ²ß ÎÏÒÈ̲ÇÀÖ²¯ ÇÀÑÒÎÑÓÂÀÍÍß ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲  Ç ÓÐÀÕÓÂÀÍÍßÌ ÅÊÎÍÎ̲×Íί ÅÔÅÊÒÈÂÍÎÑÒ²

ÊÎÍÖÅÏÖÈß ÎÏÒÈÌÈÇÀÖÈÈ ÊÎÍÑÒÐÓÊÖÈÉ ÈÇ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ Ñ Ó×ÅÒÎÌ ÝÊÎÍÎÌÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ

93–98
(6)

Íàçèí Â.È.

RESEARCH OF CAPACITY OF HYDROSTATICAL BEARING OF HOB TYPE

ÄÎÑË²ÄÆÅÍÍß ÏÐÀÖÅÇÄÀÒÍÎÑÒ²  òÄÐÎÑÒÀÒÈ×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÂÒÓËÊÎÂÎÃÎ ÒÈÏÀ

ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÈ ÃÈÄÐÎÑÒÀÒÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÂÒÓËÎ×ÍÎÃÎ ÒÈÏÀ

99–104
(6)

Ãîëîùàïîâ Â.Í.,
Êîòóëüñêàÿ Î.Â.,
Ïàðàìîíîâà Ò.Í.

Òhe management of thermal state of high-power turbine cylinders according to the changing of radial gaps

ÓÏÐÀÂ˳Ííÿ ÒÅÏËÎÂèÌ Ñòàíîì ÖÈ˳ÍÄг òóðá³íè âåëèêî¿ ïîòóæíîñò³ çà Ç̳íîþ ÐÀijÀËÜÍèÕ ÇÀÇÎгÂ

ÓÏÐÀÂËÅÍÈÅ ÒÅÏËÎÂÛÌ ÑÎÑÒÎßÍÈÅÌ ÖÈËÈÍÄÐΠÒÓÐÁÈÍÛ ÁÎËÜØÎÉ ÌÎÙÍÎÑÒÈ ÏÎ ÈÇÌÅÍÅÍÈÞ ÐÀÄÈÀËÜÍÛÕ ÇÀÇÎÐÎÂ

105–108
(4)

Åâäîêèìåíêî Þ.È.,
Êèñåëü Â.Ì.,
Òêà÷åíêî Ã.Â.,
Óðþêîâ Á.À.,
Ôðîëîâ Ã.À.,
Öûãàíåíêî Â.Ñ.

STRUCTURE AND PROPERTIES OF THE NICKEL COATINGS RECEIVED FROM NOT FUSED PARTICLES BY HIGH-VELOCITY AIR-FUEL SPRAYING

ÑÒÐÓÊÒÓÐÀ ² ÂËÀÑÒÈÂÎÑÒ² ͲÊÅËÅÂÈÕ ÏÎÊÐÈÒÒ²Â, ÎÒÐÈÌÀÍÈÕ  Ç ÍÅÐÎÇÏËÀÂËÅÍÈÕ ×ÀÑÒÈÍÎÊ ÂÈÑÎÊÎØÂÈÄʲÑÍÈÌ  ÏβÒÐßÍÎ-ÏÀËÈÂÍÈÌ ÍÀÏÈËÅÍÍßÌ

ÑÒÐÓÊÒÓÐÀ È ÑÂÎÉÑÒÂÀ ÍÈÊÅËÅÂÛÕ ÏÎÊÐÛÒÈÉ, ÏÎËÓ×ÅÍÍÛÕ ÈÇ ÍÅÐÀÑÏËÀÂËÅÍÍÛÕ ×ÀÑÒÈÖ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÛÌ ÂÎÇÄÓØÍÎ-ÒÎÏËÈÂÍÛÌ ÍÀÏÛËÅÍÈÅÌ

109–114
(6)

Ñíåæíîé Ã.Â.,
Ñàæíåâ Â.Í.

The magnetic state of AUSTENITIC MATRIX AND MECHANICAL PROPERTIES high-manganese steel

Ìàãí²òíÈÉ ñÒÀÍ àóñòåí²òíî¯ ìàòðèö² ² ìåõàí²÷Ͳ ÂËÀÑÒÈÂÎÑÒ²  âÈñîêîìàÍÃÀÍÎÂÈÕ ÊÐÈÖÜ

ÌÀÃÍÈÒÍÎÅ ÑÎÑÒÎßÍÈÅ ÀÓÑÒÅÍÈÒÍÎÉ ÌÀÒÐÈÖÛ È ÌÅÕÀÍÈ×ÅÑÊÈÅ ÑÂÎÉÑÒÂÀ ÂÛÑÎÊÎÌÀÐÃÀÍÖÅÂÛÕ ÑÒÀËÅÉ

115–120
(6)

Ïîâãîðîäíèé Â.Î.

The determinanion of the thermomechanical characteristics including solution invers problem of thermoelasticity

Âèçíà÷åííÿ òåðìîìåõàí³÷íèõ õàðàêòåðèñòèê ìàòåð³àë³â  íà îñíîâ³ ðîçâ’ÿçêó îáåðíåíèõ çàäà÷ òåðìîïðóæíîñò³

ÎÏÐÅÄÅËÅÍÈÅ ÒÅÐÌÎÌÅÕÀÍÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÀÒÅÐÈÀËΠÍÀ ÎÑÍÎÂÅ ÐÅØÅÍÈß ÎÁÐÀÒÍÛÕ ÇÀÄÀ× ÒÅÐÌÎÓÏÐÓÃÎÑÒÈ

121–126
(6)

Âåäü Â.Å.,
Ãóñåâ Þ.À.,
Ãóñåâà Í.È.,
Êàìáèç Êàõðàè

HEAT-RESISTANT COATING FOR GTE TURBINE BLADES

ÆÀÐÎÑÒ²ÉÊÅ ÏÎÊÐÈÒÒß ÄËß ËÎÏÀÒÎÊ ÒÓÐÁ²Í ÃÒÄ

ÆÀÐÎÑÒÎÉÊÎÅ ÏÎÊÐÛÒÈÅ ÄËß ËÎÏÀÒÎÊ ÒÓÐÁÈÍ ÃÒÄ

127–131
(5)

Çèíüêîâñêèé À.Ï.,
Òîêàðü È.Ã.,
Êðóö Â.À.,
Êðóãëèé ß.Ä.

INFLUENCE OF DISSIPATION OF ENERGY IN MATERIAL ON VIBRATIONS OF STRUCTURAL ELEMENTS WITH NONUNIFORMITIES

Âïëèâ ðîçñ³þâàííÿ åíåð㳿 â ìàòåð³àë³ íà êîëèâàííÿ  êîíñòðóêòèâíèõ åëåìåíò³â ç íåîäíîð³äíîñòÿìè

ÂËÈßÍÈÅ ÐÀÑÑÅßÍÈß ÝÍÅÐÃÈÈ Â ÌÀÒÅÐÈÀËÅ ÍÀ ÊÎËÅÁÀÍÈß ËÎÏÀÒÎÊ Ñ ÍÅÎÄÍÎÐÎÄÍÎÑÒßÌÈ

132–137
(6)

Êàðà÷óí Â.Â.,
Ìåëüíèê Â.Í.

CYCLIC AND AXIS NON-SYMMATRICAL COVER DEFORMATION IN THE ACOUSTIC FIELD

ÖÈÊ˲×ÍÀ ² ÎÑÅÍÅÑÈÌÅÒÐÈ×ÍÀ ÄÅÔÎÐÌÀÖ²ß ÎÁÎËÎÍÊÈ   ÀÊÓÑÒÈ×ÍÎÌÓ ÏÎ˲

ÖÈÊËÈ×ÅÑÊÀß È ÎÑÅÍÅÑÈÌÌÅÒÐÈ×ÍÀß ÄÅÔÎÐÌÀÖÈß ÎÁÎËÎ×ÊÈ Â ÀÊÓÑÒÈ×ÅÑÊÎÌ ÏÎËÅ

138–141
(4)

Õîðîëüñêèé Ï.Ã.,
Äóáîâèê Ë.Ã.,
Êóðèííîé Â.Â.

TO SELECTION OF THE LAUNCH VEHICLE FOR INJECTION TO THE INITIAL ORBITDEBRIS collector space vehicle

ÄÎ ÂÈÁÎÐÓ ÐÀÊÅÒÈ-ÍÎÑ²ß ÄËß ÄÎÑÒÀÂÊÈ ÍÀ ÂÈÕ²ÄÍÓ ÎÐÁ²ÒÓÑ̲ÒÒªÇÁÈÐÀËÜÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÀ

Ê ÂÛÁÎÐÓ ÐÀÊÅÒÛ-ÍÎÑÈÒÅËß ÄËß ÄÎÑÒÀÂÊÈ ÍÀ ÈÑÕÎÄÍÓÞ ÎÐÁÈÒÓ ÌÓÑÎÐÎÑÎÁÈÐÀÞÙÅÃÎ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÀÏÏÀÐÀÒÀ

142–145
(4)

Çàäîíöåâ Â.À.

TWO LIVES AND TWO ROCKETS OF WERNER VON BRAUN (1912-1977). TO THE 100TH ANNIVERSARY OF HIS BIRTH

ÄÂÀ ÆÈÒÒß ÒÀ IJ ÐÀÊÅÒÈ ÂÅÐÍÅÐÀ ÔÎÍ ÁÐÀÓÍÀ (1912-1977).  ÄÎ 100-в××ß ²Ç ÄÍß ÍÀÐÎÆÄÅÍÍß

ÄÂÅ ÆÈÇÍÈ È ÄÂÅ ÐÀÊÅÒÛ ÂÅÐÍÅÐÀ ÔÎÍ ÁÐÀÓÍÀ (1912-1977). Ê 100-ËÅÒÈÞ ÑÎ ÄÍß ÐÎÆÄÅÍÈß

146–158
(13)

Ðåâà Â.Ñ.,
Ôðîëîâ Â.Ï.,
Çåìëÿíîé Ê.Í.,
Øåâ÷åíêî Å.Þ.

JUSTIFICATION FOR PRODUCTION AND ELECTRIC POWER QUALITY CONTROL SYSTEM STRUCTURE AS PART OF GROUND COMPLEX POWER SUPPLY SYSTEM

ÎÁ¥ÐÓÍÒÓÂÀÍÍß ÍÅÎÁÕ²ÄÍÎÑÒ² ÑÒÂÎÐÅÍÍß  ² ÑÒÐÓÊÒÓÐÀ  ÑÈÑÒÅÌÈ ÊÎÍÒÐÎËÞ ßÊÎÑÒ² ÅËÅÊÒÐÎÅÍÅÐò¯   Ó ÑÊËÀIJ ÑÈÑÒÅÌÈ ÅËÅÊÒÐÎÏÎÑÒÀ×ÀÍÍß  ÍÀÇÅÌÍÎÃÎ ÊÎÌÏËÅÊÑÓ

ÎÁÎÑÍÎÂÀÍÈÅ ÍÅÎÁÕÎÄÈÌÎÑÒÈ ÑÎÇÄÀÍÈß È ÑÒÐÓÊÒÓÐÀ ÑÈÑÒÅÌÛ ÊÎÍÒÐÎËß ÊÀ×ÅÑÒÂÀ ÝËÅÊÒÐÎÝÍÅÐÃÈÈ Â ÑÎÑÒÀÂÅ ÑÈÑÒÅÌÛ ÝËÅÊÒÐÎÑÍÀÁÆÅÍÈß ÍÀÇÅÌÍÎÃÎ ÊÎÌÏËÅÊÑÀ

159–162
(4)

Êîíîõ Â.È.,
Êàëèíè÷åíêî È.È.,
Ãîðäèåö È.Í.,
Êóêñà È.Þ.

The FEATURES OF MATHEMATICAL MODELING OF WORKING PROCESSES IN HYDRAULIC POWER systems WITH a PNEUMATIC ACTUATOR

Îñîáëèâîñò³ ìàòåìàòè÷íîãî ìîäåëþâàííÿ ðîáî÷èõ ïðîöåñ³â  â ÄÆÅÐÅËÀÕ Ã²äðàâë³÷íî¿ ïîòóæíîñò³  ç ïíåâìàòè÷íèì ïîâ³äíèêîì

ÎÑÎÁÅÍÍÎÑÒÈ ÌÀÒÅÌÀÒÈ×ÅÑÊÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÐÀÁÎ×ÈÕ ÏÐÎÖÅÑÑΠ ÈÑÒÎ×ÍÈÊÀÕ ÃÈÄÐÀÂËÈ×ÅÑÊÎÉ ÌÎÙÍÎÑÒÈ Ñ ÏÍÅÂÌÀÒÈ×ÅÑÊÈÌ ÏÐÈÂÎÄÎÌ

163–168
(6)

Êîâàëåíêî À.Í.,
Áëèøóí Þ.Â.,
Êèðñàíîâ Ä.Â.,
Íèêèùåíêî È.Í.,
Ñêà÷êî Â.Ñ.

Rated evaluation of factors that affect the gas-dynamic launch during high-altitude engine test

ÐÎÇÐÀÕÓÍÊÎÂÀ ÎÖ²ÍÊÀ ÔÀÊÒÎв ÙÎ ÂÏËÈÂÀÞÒÜ ÍÀ ÇÀÏÓÑÊ  ãàçîäèíàì³÷íî¿ òðóáè Ï²Ä ×ÀÑ ÂÈÏÐÎÁÓÂÀÍÍß ÂÈÑÎÒÍÎÃÎ ÄÂÈÃÓÍÀ

ÐÀÑ×ÅÒÍÀß ÎÖÅÍÊÀ ÔÀÊÒÎÐÎÂ, ÂËÈßÞÙÈÕ ÍÀ ÇÀÏÓÑÊ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÒÐÓÁÛ ÏÐÈ ÈÑÏÛÒÀÍÈÈ ÂÛÑÎÒÍÎÃÎ ÄÂÈÃÀÒÅËß

169–173
(5)

Èâ÷åíêî Ë.Ô.,
Äåøåâûõ Ñ.À.,
Ìàêñèì÷óê Ð.Ô.

EXPERIENCE OF DESIGNING OF THE autonomous TURBINE TPU ENGINE RD861K

ÄÎÑÂ²Ä ÏÐÎÅÊÒÓÂÀÍÍß ÀÂÒÎÍÎÌÍί ÒÓÐÁ²ÍÈ ÒÍÀ ÄÂÈÃÓÍÀ ÐÄ861Ê

ÎÏÛÒ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÀÂÒÎÍÎÌÍÎÉ ÒÓÐÁÈÍÛ ÒÍÀ ÄÂÈÃÀÒÅËß ÐÄ861Ê

174–179
(6)

Ïîìèí Î.Â.,
Ëÿõ Þ.À.,
Êîðîëåâ Â.Ã.,
Áå
ñêðîâíûé È.Á.,
Ëüíÿíîé Â.Í.

EXPERIENCE OF THE ENTERPRISE FOR CLEARING INTERNAL HEAT-SHIELDING COVERING ROCKET ENGINES OF FIRM FUEL AFTER THE WORK TERMINATION AT CARRYING OUT OF BENCH TESTS

Äîñâ³ä ï³äïðèºìñòâà ïî ãàñ³ííþ âíóòð³øíüîãî òåïëîçàõèñíîãî  ïîêðèòòÿ ðàêåòíèõ äâèãóí³â òâåðäîãî ïàëèâà ï³ñëÿ çàê³í÷åííÿ ðîáîòè  ïðè ïðîâåäåíí³ ñòåíäîâèõ âèïðîáóâàíü

ÎÏÛÒ ÏÐÅÄÏÐÈßÒÈß ÏÎ ÃÀØÅÍÈÞ ÂÍÓÒÐÅÍÍÅÃÎ ÒÅÏËÎÇÀÙÈÒÍÎÃÎ ÏÎÊÐÛÒÈß ÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÒÂÅÐÄÎÃÎ ÒÎÏËÈÂÀ ÏÎÑËÅ ÎÊÎÍ×ÀÍÈß ÐÀÁÎÒÛ ÏÐÈ ÏÐÎÂÅÄÅÍÈÈ ÑÒÅÍÄÎÂÛÕ ÈÑÏÛÒÀÍÈÉ

180–184
(5)

Äàâèäîâ À.Î.

THE ACADEMIC QUESTIONS OF PROLONGATION OF LIFE TIME OF ELECTROCHEMICAL BATTERIES IN POWER INSTALLATIONS OF SPACE-ROCKET OBJECTS

ÎÑÍÎÂͲ ÅÒÀÏÈ ÄÎÑË²ÄÆÅÍÜ ÏÎ ÇÀÁÅÇÏÅ×ÅÍÍÞ ÒÐÈÂÀËÎÃÎ ÐÅÑÓÐÑÓ  ÅËÅÊÒÐÎղ̲×ÍÈÕ ÀÊÓÌÓËßÒÎв  ÅÍÅÐÃÎÓÑÒÀÍÎÂÊÀÕ  ÐÀÊÅÒÍÎ-ÊÎÑ̲×ÍÈÕ ÎÁ’ªÊÒ²Â

ÎÑÍÎÂÍÛÅ ÝÒÀÏÛ ÈÑÑËÅÄÎÂÀÍÈÉ ÏÎ ÎÁÅÑÏÅ×ÅÍÈÞ ÄËÈÒÅËÜÍÎÃÎ ÐÅÑÓÐÑÀ ÝËÅÊÒÐÎÕÈÌÈ×ÅÑÊÈÕ ÀÊÊÓÌÓËßÒÎÐΠ ÝÍÅÐÃÎÓÑÒÀÍÎÂÊÀÕ ÐÀÊÅÒÍÎ-ÊÎÑÌÈ×ÅÑÊÈÕ ÎÁÚÅÊÒÎÂ

185–190
(6)

Öàãëîâ À.È.

PLUME PARAMETERS INVESTIGATION OF ELECTRODELESS ELECTRIC PROULSION THRUSTER WITH RF IONSZATION OF WORKING MEDIUM

ÄÎÑË²ÄÆÅÍÍß ÏÀÐÀÌÅÒв ÑÒÐÓ¯ ÁÅÇÅËÅÊÒÐÎÄÍÎÃÎ ÅÐÄ Ç Â× ²ÎͲÇÀÖ²ªÞ ÐÒ

ÈÑÑËÅÄÎÂÀÍÈÅ ÏÀÐÀÌÅÒÐΠÑÒÐÓÈ ÁÅÇÝËÅÊÒÐÎÄÍÎÃÎ ÝÐÄ Ñ Â× ÈÎÍÈÇÀÖÈÅÉ ÐÒ

191–195
(5)

Òèòîâ Ì. Þ.,
Äåîï Ô.,
Æèáåð Ò.,
Ëîÿí À.Â.

Ions speed measuring in plasma beam of low-power Hall Effect thruster SPT-20M using laser-induced fluorescence velocimetry

ÂÈ̲РØÂÈÄÊÎÑÒÅÉ ²ÎͲ  Ïëàçìîâîìó ïó÷êó Õîëëîâñüêîãî ÄÂÈÃÓÍÀ ÌÀËί ÏÎÒÓÆÍÎÑÒ² ÑÏÄ-20Ì ÌÅÒÎÄÎÌ  ËÀÇÅÐÍÎ-³íäóêîâàíî¿ ôëóîðåñöåíö³¿

ÈÇÌÅÐÅÍÈÅ ÑÊÎÐÎÑÒÅÉ ÈÎÍÎÂ Â ÏËÀÇÌÅÍÍÎÉ ÑÒÐÓÅ  ÕÎËËÎÂÑÊÎÃÎ ÄÂÈÃÀÒÅËß ÌÀËÎÉ ÌÎÙÍÎÑÒÈ ÑÏÄ-20Ì ÌÅÒÎÄÎÌ ËÀÇÅÐÍÎ-ÈÍÄÓÖÈÐÎÂÀÍÍÎÉ ÔËÓÎÐÅÑÖÅÍÖÈÈ

196–200
(5)

Àãååâà Å.Ã.,
Ëîÿí À.Â.,
Ãàéäóêîâ Â.Ô.

EXPERIMENTALLY RESEARCH OF SELFHEATED HOLLOW CATHODE EROSION BY OPTICAL SPECTROSCOPY METHOD

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÅÐÎDz¯ ÁÅÇÍÀ×ÀËÜÍÎÃÎ ÏÎÐÎÆÍÈÑÒÎÃÎ ÊÀÒÎÄÀ ÌÅÒÎÄÎÌ ÎÏÒÈ×Íί Å̲ѲÉÍί ÑÏÅÊÒÐÎÑÊÎϲ¯

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÝÐÎÇÈÈ ÁÅÇÍÀÊÀËÜÍÎÃÎ ÏÎËÎÃÎ ÊÀÒÎÄÀ ÌÅÒÎÄÎÌ ÎÏÒÈ×ÅÑÊÎÉ ÝÌÈÑÑÈÎÍÍÎÉ ÑÏÅÊÒÐÎÑÊÎÏÈÈ

201–205
(5)

Õèòüêî À.Â.,
Ìàñëÿíûé Í.Â.

HOLLOW CATHODES OF ELECTRIC PROPULSION NON-CLASSICAL  SCHEMES

ÏÎÐÎÆÍÈÑÒ² ÊÀÒÎÄÈ ÅËÅÊÒÐÈ×ÍÈÕ ÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲÂÍÅÊËÀÑÈ×Íί ÑÕÅÌÈ

ÏÎËÛÅ ÊÀÒÎÄÛ ÝËÅÊÒÐÈ×ÅÑÊÈÕ ÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÅÊËÀÑÑÈ×ÅÑÊÎÉ ÑÕÅÌÛ

206–209
(4)

×åðêóí À.Ì.

RESEARCH METHOD OF PLASMA DOUBLE LAYER INFLUENCE ON HOLLOW CATHODE’S GAS EFFICIENCY

ÌÅÒÎÄÈÊÀ ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÏÎIJÉÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ØÀÐÓ  ÍÀ ÃÀÇÎÂÓ ÅÔÅÊÒÈÂͲÑÒÜ ÏÎÐÎÆÍÈÍÍÎÃÎ ÊÀÒÎÄÀ

ÌÅÒÎÄÈÊÀ ÈÑÑËÅÄÎÂÀÍÈß ÂËÈßÍÈß ÄÂÎÉÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÑËÎß ÍÀ ÃÀÇÎÂÓÞ ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÏÎËÎÃÎ ÊÀÒÎÄÀ

210–213
(4)

Óìàíñêèé À.Ï.,
Ñòîðîæåíêî Ì.Ñ.,
Àêîïÿí Â.Â.,
Ìàðöåíþê È.Ñ.

STEEL HARDENING BY ELECTRIC-SPARK ALLOYING WITH COMPOSITE MATERIALS OF TiB2-(Fe-Mo) SYSTEM

ÅËÅÊÒÐβÑÊÐÎÂÅ Ç̲ÖÍÅÍÍß ÑÒÀ˲  ÊÎÌÏÎÇÈÖ²ÉÍÈÌÈ ÌÀÒÅвÀËÀÌÈ ÑÈÑÒÅÌÈ TiB2-(Fe-Mo)

ÝËÅÊÒÐÎÈÑÊÐÎÂÎÅ ÓÏÐÎ×ÍÅÍÈÅ ÑÒÀËÈ ÊÎÌÏÎÇÈÖÈÎÍÍÛÌÈ ÌÀÒÅÐÈÀËÀÌÈ ÑÈÑÒÅÌÛ TiB2-(Fe-Mo)

214–218
(5)

Á³ëÿêîâè÷ Î.Ì.,
Êóðáåò Ë.Â.,
Áîãàéñüêà Ê.Â.

RESEARCH OF LUBRICATION EFFECT EFFECIENCY OF THE TRANSMISSION OILS IN THE CONDITIONS OF THE PROTRACTED EXPLOITATION AT STATIONARE MODES OF FRICTION

ÄÎÑË²ÄÆÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÌÀÑÒÈËÜÍί IJ¯ ÒÐÀÍÑ̲ѲÉÍÈÕ ÎËÈ  ÓÌÎÂÀÕ ÒÐÈÂÀËί ÅÊÑÏËÓÀÒÀÖ²¯ ÏÐÈ ÑÒÀÖ²ÎÍÀÐÍÈÕ ÐÅÆÈÌÀÕ ÒÅÐÒß

ÈÑÑËÅÄÎÂÀÍÈÅ ÝÔÅÊÒÈÂÍÎÑÒÈ ÑÌÀÇÛÂÀÞÙÅÃÎ ÄÅÉÑÒÂÈß
ÒÐÀÍÑÌÈÑÑÈÎÍÍÛÕ ÌÀÑÅË Â ÓÑËÎÂÈßÕ ÄËÈÒÅËÜÍÎÉ ÝÊÑÏËÓÀÒÀÖÈÈ ÏÐÈ ÑÒÀÖÈÎÍÀÐÍÛÕ ÐÅÆÈÌÀÕ ÒÐÅÍÈß

219–223
(5)

Ðÿáêîâ Â.È.,
Òîëìà÷åâ Í.Ã.

SUPERSYMMETRIC MODEL IN RESEARCH OF MATTER PROPERTIES

CÓÏÅÐÑÈÌÅÒÐÈ×ÍÀ ÌÎÄÅËÜ Ó ÄÎÑË²ÄÆÅÍͲ ÂËÀÑÒÈÂÎÑÒÅÉ ÐÅ×ÎÂÈÍÈ

ÑÓÏÅÐÑÈÌÌÅÒÐÈ×ÍÀß ÌÎÄÅËÜ Â ÈÑÑËÅÄÎÂÀÍÈÈ ÑÂÎÉÑÒ ÂÅÙÅÑÒÂÀ

224–228
(5)

Èíôîðìàöèîííûå òåõíîëîãèè

Ìèðãîðîä Â.Ô.,
Ãâîçäåâà È.Ì.,
Äàíèëîâ Â.Â.,
Áóðÿ÷åíêî À.Ã.,
Âîëêîâ Ä.È.

METHODS OF NUMERICAL REALIZATION OF MATHEMATICAL MODELS OF DYNAMICAL PROCESSES IN THE FORM OF INTEGRAL EQUATION

ÌÅÒÎÄÈ ×ÈÑÅËÜÍί ÐÅÀ˲ÇÀÖ²¯  ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÄÈÍÀ̲×ÍÈÕ ÏÐîÖÅѲ  Ó ÔÎÐ̲ ²ÍÒÅÃÐÀËÜÍÈÕ Ð²ÂÍßÍÜ

ÌÅÒÎÄÛ ×ÈÑËÅÍÍÎÉ ÐÅÀËÈÇÀÖÈÈ ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÄÈÍÀÌÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑΠ ÔÎÐÌÅ ÈÍÒÅÃÐÀËÜÍÛÕ ÓÐÀÂÍÅÍÈÉ

229–233
(5)

Åïèôàíîâ Ñ.Â.,
Ñèðåíêî Ô.Ô.,
Ñóõîâåé Ñ.È.,
Çåëåíñêèé Ð.Ë.

CREATING A QUICK PROCEEDING MATHEMATICAL MODEL OF A TURBOSHAFT ENGINE STARTING SIMULATION FOR AUTOMATIC CONTROL SYSTEM SYNTHESIS PURPOSES

ÑÒÂÎÐÅÍÍß ØÂÈÄÊÎÐÀÕ²ÂÍί ÌÀÒÅÌÀÒÈ×Íί ÌÎÄÅ˲  ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ÅÒÀϲ ÇÀÏÓÑÊÓ  ÄËß Ð²ØÅÍÍß ÇÀÄÀ× ÑÈÍÒÅÇÓ ÑÈÑÒÅÌ  ÀÂÒÎÌÀÒÈ×ÍÎÃÎ ÊÅÐÓÂÀÍÍß

ÑÎÇÄÀÍÈÅ ÁÛÑÒÐÎÑ×ÅÒÍÎÉ ÌÀÒÅÌÀÒÈ×ÅÑÊÎÉ ÌÎÄÅËÈ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÀÒÅËß ÍÀ ÝÒÀÏÅ ÇÀÏÓÑÊÀ ÄËß ÐÅØÅÍÈß ÇÀÄÀ× ÑÈÍÒÅÇÀ ÑÈÑÒÅÌ ÀÂÒÎÌÀÒÈ×ÅÑÊÎÃÎ ÓÏÐÀÂËÅÍÈß

234–242
(9)

Òàðàñåíêî À.È.,
Òàðàñåíêî À.À.

full-range dynamic GTE model

øèðîêîäèàïàçîííà ÄÈÍÀ̲÷íà ìîäåëü ãòä

ØÈÐÎÊÎÄÈÀÏÀÇÎÍÍÀß ÄÈÍÀÌÈ×ÅÑÊÀß ÌÎÄÅËÜ ÃÒÄ

243–247
(5)

Ìàðàâèëëà Ýððåðà Ê.

ANALYSIS OF THE EFFECTIVESS OF ALTERNATIVE MODELS TO PREDICT THE COEFFICIENTS OF HEAT EXCHANGE ON THE BLADE EXTERNAL SURFACE TAKING I NTO ACCONT THE ENGINE IDIVIDUAL CHARACTERISTICS

àíàë³ç åôåêòèâíîñò³ ÷îòèðüîõ ð³çíèõ ìîäåëåé  äëÿ âèçíà÷åííÿ êîåô³ö³ºíò³â òåïëîâ³ääà÷³  íà çîâí³øí²é ïîâåðõí³ ëîïàòêè ç ÓÐÀÕóÂÀÍÍßÌ  âïëèâó ³íäèâ³äóàëüíèõ õàðàêòåðèñòèê äâèãóí³â

ÀÍÀËÈÇ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÀËÜÒÅÐÍÀÒÈÂÍÛÕ ÌÎÄÅËÅÉ ÄËß ÎÏÐÅÄÅËÅÍÈß ÊÎÝÔÔÈÖÈÅÍÒΠÒÅÏËÎÎÒÄÀ×È ÍÀ ÍÀÐÓÆÍÎÉ ÏÎÂÅÐÕÍÎÑÒÅÉ ËÎÏÀÒÊÈ Ñ Ó×ÅÒÎÌ ÈÍÄÈÂÈÄÓÀËÜÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÄÂÈÃÀÒÅËß

248–252
(5)

Âàñèëåíêî À.È.,
Êîñòÿí È.È.,
Ñåðãååâ Ñ.Ï.

FORMING OF CHANNELS FAILURE CRITERION FOR MEASURING GAS TURBINE ENGINE PARAMETERS AND ACS RESPONSE

ÔÎÐÌÓÂÀÍÍß ÎÇÍÀÊ Â²ÄÌÎÂÈ ÊÀÍÀ˲ ÂÈ̲ÐÞÂÀÍÍß ÏÀÐÀÌÅÒв  ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ ² ÐÅÀÊÖ²¯ ÍÀ ÍÜÎÃÎ ÑÀÊ ³ Ð ÀÃÐÅÃÀÒÓ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÏÐÈÇÍÀÊÎÂ ÎÒÊÀÇÀ ÊÀÍÀËÎÂ ÈÇÌÅÐÅÍÈß ÏÀÐÀÌÅÒÐÎÂ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß È ÐÅÀÊÖÈß ÍÀ ÍÅÃÎ ÑÀÓÈÐ ÀÃÐÅÃÀÒÀ

253–256
(4)

Áóðàó Í.È.,
Ïàâëîâñêèé À.Ì.,
ßöêî Ë.Ë.

SIMULATION OF THE TWO-LEVELS VIBRATION CONTROL SYSTEM OF AVIATION ENGINE BY USING NI  LABVIEW TECHNIQUE

ÌÎÄÅËÞÂÀÍÍß ÄÂÎвÂÍÅÂί ÑÈÑÒÅÌÈ ÊÎÍÒÐÎËÞ  ²ÁÐÀÖ²¯ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ   ÑÈÑÒÅ̲ NI  LABVIEW

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÄÂÓÕÓÐÎÂÍÅÂÎÉ ÑÈÑÒÅÌÛ ÊÎÍÒÐÎËß ÂÈÁÐÀÖÈÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß Â  ÑÈÑÒÅÌÅ NI LABVIEW

257–262
(6)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Øîñòàê È.Â.,
ßíîâñêàÿ Ê.Ý.,
Ðîññîõà Ñ.Â.

AUTOMATION OF PROCESS FORMING SHEDULED OF LESSONS BASED ON THE TENSOR IN TRAINING COMPLEX

ÀÂÒÎÌÀÒÈÇÀÖ²ß ÏÐÎÖÅÑÓ ÑÊËÀÄÀÍÍß ÐÎÇÊËÀÄÓ ÇÀÍßÒÜ  ÍÀ ÎÑÍβ ÒÅÍÇÎÐÍÎÃΠ ÎÁ×ÈÑËÅÍÍß   Ó×ÁÎÂÎÌÓ ÊÎÌÏËÅÊѲ

ÀÂÒÎÌÀÒÈÇÀÖÈß ÏÐÎÖÅÑÑÀ ÑÎÑÒÀÂËÅÍÈß ÐÀÑÏÈÑÀÍÈß ÇÀÍßÒÈÉ ÍÀ ÎÑÍÎÂÅ ÒÅÍÇÎÐÍÎÃÎ ÈÑ×ÈÑËÅÍÈß Â Ó×ÅÁÍÎÌ ÊÎÌÏËÅÊÑÅ

263–266
(4)

Ïîòàïîâà Ì.Â.

SYSTEM MODEL OF SCHEDULING OF PROGRAM PROJECTS

ÑÈÑÒÅÌÍÀ ÌÎÄÅËÜ ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÓÂÀÍÍß ÏÐÎÃÐÀÌÍÈÕ ÏÐÎÅÊÒ²Â

ÑÈÑÒÅÌÍÀß ÌÎÄÅËÜ ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÈÐÎÂÀÍÈß ÏÐÎÃÐÀÌÌÍÛÕ ÏÐÎÅÊÒÎÂ

267–272
(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).