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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2013. – ¹ 8(105). – 294 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 8(105). – 294ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 8(105). – 294 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Æóëàé Þ.À.,
Ñêîñàðü Â.Þ.

HYDRODYNAMIC CAVITATION AS A TOOL TO INTENSIFY PRODUCTION PROCESSES. XPERIENCE OF USAGE AND PROSPECTS  (REVIEW)

ÊÀ²ÒÀֲߠ ßÊ ÇÀѲÁ ²ÍÒÅÍÑÈÔ²ÊÀÖ²¯ ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲÂ. ÄÎÑÂ²Ä ÇÀÑÒÎÑÓÂÀÍÍß É ÏÅÐÑÏÅÊÒÈÂÈ  (ÎÃËßÄ)

ÊÀÂÈÒÀÖÈß ÊÀÊ ÑÐÅÄÑÒÂÎ ÈÍÒÅÍÑÈÔÈÊÀÖÈÈ ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÕ ÏÐÎÖÅÑÑÎÂ. ÎÏÛÒ ÏÐÈÌÅÍÅÍÈß È ÏÅÐÑÏÅÊÒÈÂÛ (ÎÁÇÎÐ)

7–15
(
9)

Íàáîêèíà Ò.Ï.,
Ãàéäà÷óê À.Â.,
Ãðóøåíêî À.Ì.

INCREASE OF TECHNOLOGICAL EQUIPMENT CLEANING EFFICIENCY OF thermogas dynamic METHOD AT PRODUCTION OF GTÅ SHOULDER-BLADES

²ÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² Î×ÈÙÅÍÍß ÒÅÕÍÎËÎò×ÍÎÃÎ ÎÁËÀÄÍÀÍÍß ÒÅÐÌÎÃÀÇÎÄÈÍÀ̲×ÍÈÌ ÌÅÒÎÄÎÌ ÏÐÈ ÂÈÐÎÁÍÈÖÒ² ËÎÏÀÒÎÊ ÃÒÄ

ÏÎÂÛØÅÍÈÅ ÝÔÔÅÊÒÈÂÍÎÑÒÈ Î×ÈÑÒÊÈ ÒÅÕÍÎËÎÃÈ×ÅÑÊÎÃÎ ÎÁÎÐÓÄÎÂÀÍÈß ÒÅÐÌÎÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÈÌ ÌÅÒÎÄÎÌ ÏÐÈ ÏÐÎÈÇÂÎÄÑÒÂÅ ËÎÏÀÒÎÊ ÃÒÄ

16–20
(
5)

Êëèìåíêî Ë.Ï.,
Àíäðººâ Â.².,
Äèõòà Ë.Ì.,
Ïðèùåïîâ Î.Ô.

THERMO-INSULATION COVERAGES OF WORKING SURFACE OF POROUS CASTING FORMS ARE FOR CASTING OF SHELLS OF CYLINDERS OF ENGI

ÒÅÐÌβÇÎËßÖ²ÉͲ ÏÎÊÐÈÒÒß ÐÎÁÎ×ί ÏÎÂÅÐÕͲ ÏÎÐÈÑÒÈÕ ËÈÂÀÐÍÈÕ ÊÎʲ˲ ÄËß ËÈÒÒß Ã²ËÜÇ ÖÈ˲ÍÄв ÄÂÇ

ÒÅÐÌÎÈÇÎËßÖÈÎÍÍÛÅ ÏÎÊÐÛÒÈß ÐÀÁÎ×ÅÉ ÏÎÂÅÐÕÍÎÑÒÈ ÏÎÐÈÑÒÛÕ ËÈÒÅÉÍÛÕ ÊÎÊÈËÅÉ ÄËß ËÈÒÜß ÃÈËÜÇ ÖÈËÈÍÄÐΠÄÂÑ

21–24
(
4)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Óëèòåíêî Þ.À.,
Åëàíñêèé À.Â.,
Êðàâ÷åíêî È.Ô.

PROBLEMS OF SELECTION OF CONFIGURATION FOR POWERPLANT INTENDED FOR SPACE TRANSPORTATION SYSTEM STAGE 1

ÏðîáëåìÈ âÈáîðÓ ñõåìÈ ñèëîâî¯ óñòàíîâêè äëÿ ÏÅÐØÎ¯ ñòóïåí² òðàíñïîðòíî-ÊÎÑ̲×Íί ñèñòåìÈ

ÏÐÎÁËÅÌÛ ÂÛÁÎÐÀ ÑÕÅÌÛ ÑÈËÎÂÎÉ ÓÑÒÀÍÎÂÊÈ ÄËß ÏÅÐÂÎÉ ÑÒÓÏÅÍÈ ÒÐÀÍÑÏÎÐÒÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ

25–30
(
6)

Ïîâãîðîäíèé Â.Î.

IDENTIFICATION OF THE PARAMETER’S OF THERMOELASTICITY TO THE NONHOMOGENEOUS STRESS CONDITION ON THE SOLUTION INVERSE PROBLEM OF THE THERMOELASTICITY

²ÄÅÍÒÈÔ²ÊÀÖ²ß ÏÀÐÀÌÅÒв ÒÅÐÌÎÏÐÓÆÍÎÑÒ² ÒÎÍÊÎÑÒ²ÍÍÈÕ ÑÈÑÒÅÌ ÏÐÈ ÍÅÎÄÍÎвÄÍÎÌÓ ÍÀÏÐÓÆÅÍÎ-ÄÅÔÎÐÌÎÂÀÍÎÌÓ ÑÒÀͲ ÍÀ ÎÑÍβ ÂÈвØÅÍÍß ÎÁÅÐÍÅÍÈÕ ÇÀÄÀ× ÒÅÐÌÎÏÐÓÆÍÎÑÒ²

ÈÄÅÍÒÈÔÈÊÀÖÈß ÏÀÐÀÌÅÒÐΠÒÅÐÌÎÓÏÐÓÃÎÑÒÈ ÒÎÍÊÎÑÒÅÍÍÛÕ ÑÈÑÒÅÌ ÏÐÈ ÍÅÎÄÍÎÐÎÄÍÎÌ ÍÀÏÐ߯ÅÍÍÎ-ÄÅÔÎÐÌÈÐÎÂÀÍÍÎÌ ÑÎÑÒÎßÍÈÈ ÍÀ ÎÑÍÎÂÅ ÐÅØÅÍÈß ÎÁÐÀÒÍÛÕ ÇÀÄÀ× ÒÅÐÌÎÓÏÐÓÃÎÑÒÈ

31–34
(
4)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Êóõòèí Þ.Ï.,
Ëàïîòêî Â.Ì.,
Ñëûíüêî Ã.È.

VERIFICATION of the numerical method For detached flows SOLUTION

ÂÅÐÈÔ²ÊÀֲߠ ÌÅÒÎÄÓ ×ÈÑÅËÜÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß Â²ÄÐÈÂÍÈÕ ÒÅ×²É ÃÀÇÓ

ÂÅÐÈÔÈÊÀÖÈß ÌÅÒÎÄÀ ×ÈÑËÅÍÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÎÒÐÛÂÍÛÕ ÒÅ×ÅÍÈÉ ÃÀÇÀ

35–39
(
5)

Òåðåøèí À.Ì.,
×åâàãèí À.Ô.

Deceleration of supersonic flow in pseudoshock, hydraulic diameter concepT

ÃÀËÜÌÓÂÀÍÍß ÍÀÄÇÂÓÊÎÂÎÃÎ ÏÎÒÎÊÓ Ó ÏÑÅÂÄÎÑÒÐÈÁÊÓ, ÊÎÍÖÅÏÖ²ß ÃÈÄÐÀÂ˲×ÍÎÃÎ ÄÈÀÌÅÒÐÓ

ÒÎÐÌÎÆÅÍÈÅ ÑÂÅÐÕÇÂÓÊÎÂÎÃÎ ÏÎÒÎÊÀ  ÏÑÅÂÄÎÑÊÀ×ÊÅ, ÊÎÍÖÅÏÖÈß ÃÈÄÐÀÂËÈ×ÅÑÊÎÃÎ ÄÈÀÌÅÒÐÀ

40–45
(
6)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ùèïàêîâ Â.À.

DESIGN AND EXPERIMENTAL ANALYSIS OF THE TURBOCOMPRESSOR UNIT WITH PULSSATING GAS DYNAMIC RESONATORS

ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÒÓÐÁÎÊÎÌÏÐÅÑÎÐÍÎÃÎ ÀÃÐÅÃÀÒÓ Ç ÁËÎÊÎÌ ÏÓËÜÑÓÞ×ÈÕ ÃÀÇÎÄÈÍÀ̲×ÍÈÕ ÐÅÇÎÍÀÒÎвÂ

ÐÀÑ×ÅÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÒÓÐÁÎÊÎÌÏÐÅÑÑÎÐÍÎÃÎ ÀÃÐÅÃÀÒÀ Ñ ÁËÎÊÎÌ ÏÓËÜÑÈÐÓÞÙÈÕ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÐÅÇÎÍÀÒÎÐÎÂ

46–50
(
5)

Áèëåêà Á.Ä.,
Êàáêîâ Â.ß.,
Ñåðãèåíêî Ð.Â.

ABOUT USING PROPANE IN THE POWER THERMODYNAMIC CYCLE WITH ISOTHERMAL COMPRESSION OF WORKING MEDIUM IN POWER UNIT WHICH UTILIZE WASTE HEAT

 

ÄÎ ÂÈÊÎÐÈÑÒÀÍÍß ÏÐÎÏÀÍÓ Ó ÑÈËÎÂÎÌÓ ÒÅÐÌÎÄÈÍÀ̲×ÍÎÌÓ ÖÈÊ˲ Ç ²ÇÎÒÅÐ̲×ÍÈÌ ÑÒÈÑÍÅÍÍßÌ ÐÎÁÎ×ÎÃÎ Ò²ËÀ  ÒÅÏËÎÓÒÈ˲ÇÀÖ²ÉÍ²É ÅÍÅÐÃÎÓÑÒÀÍÎÂÖ²

Ê ÈÑÏÎËÜÇÎÂÀÍÈÞ ÏÐÎÏÀÍÀ  ÑÈËÎÂÎÌ ÒÅÐÌÎÄÈÍÀÌÈ×ÅÑÊÎÌ ÖÈÊËÅ Ñ ÈÇÎÒÅÐÌÈ×ÅÑÊÈÌ ÑÆÀÒÈÅÌ ÐÀÁÎ×ÅÃÎ ÒÅËÀ  ÒÅÏËÎÓÒÈËÈÇÈÐÓÞÙÅÉ ÝÍÅÐÃÎÓÑÒÀÍÎÂÊÅ

51–56
(
6)

Ìàòâååíêî Â.Ò.,
Î÷åðåòÿíûé Â.À.,
Ãîðîáåö Ã.Â.

POWER BOOST GAS TURBINE ENGINES COMPLETE CYCLES, HEAT RECOVE

ÔÎÐÑÓÂÀÍÍß ÏÎÒÓÆÍÎÑÒ² ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ ÑÊËÀÄÍÎÃÎ ÖÈÊËÓ Ç ÐÅÃÅÍÅÐÀÖ²ªÞ ÒÅÏËÎÒÈ

ÔÎÐÑÈÐÎÂÀÍÈÅ ÌÎÙÍÎÑÒÈ ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÑËÎÆÍÎÃÎ ÖÈÊËÀ Ñ ÐÅÃÅÍÅÐÀÖÈÅÉ ÒÅÏËÎÒÛ

57–60
(
4)

Òêà÷ Ì.Ð.,
Òèìîøåâñêèé Á.Ã.,
Äîöåíêî Ñ.Ì.,
Ãàëûíêèí Þ.Í.

UTILIZATION OF LOW POTENTIAL HEAT THE LOW SPEED ICE FROM HYDRIDE TECHNOLOGY

ÓÒÈ˲ÇÀÖ²ß Í²ÇÊÎÏÎÒÅÍÖ²ÉÍÎÃÎ ÒÅÏËÀ ÌÀËÎÎÁÎÐÎÒÍÈÕ ÄÂÇ ÍÀ ÁÀDz òÄÐÈÄÍί ÒÅÕÍÎËÎò¯

ÓÒÈËÈÇÀÖÈß ÍÈÇÊÎÏÎÒÅÍÖÈÀËÜÍÎÃÎ ÒÅÏËÀ ÌÀËÎÎÁÎÐÎÒÍÛÕ ÄÂÑ ÍÀ ÁÀÇÅ ÃÈÄÐÈÄÍÎÉ ÒÅÕÍÎËÎÃÈÈ

61–66
(
6)

Ðàä÷åíêî Í.È.,
Ñèðîòà À.À.,
Ðàä÷åíêî Ð.Í.,
Êîíîâàëîâ Ä.Â.

COOLING POTENTIAL OF SCAVENGE AIR OF LOW SPEED DIESEL ENGINE OF TRANSPORT SHIP

ÏÎÒÅÍÖ²ÀË ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ ÏβÒÐß ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

ÏÎÒÅÍÖÈÀË ÎÕËÀÆÄÅÍÈß ÍÀÄÄÓÂÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ

67–72
(
6)

Òàðàñåíêî Ì.À.,
Òàðàñåíêî À.È.

extraneous TEMPERATURE EFFECT ON THE PARAMETERS OF AIR MODES FOR PARTIAL GTE POWER

âïëèâ òåìïåðàòóðè çîâí³øíüîãî ïîâ³òðÿ íà ïàðàìåòðè ÷àñòêîâèõ ðåæèì³â ãòä äëÿ åëåêòðîñòàíö³¿

ÂËÈßÍÈÅ ÒÅÌÏÅÐÀÒÓÐÛ ÍÀÐÓÆÍÎÃÎ ÂÎÇÄÓÕÀ ÍÀ ÏÀÐÀÌÅÒÐÛ ×ÀÑÒÈ×ÍÛÕ ÐÅÆÈÌΠÃÒÄ ÄËß ÝËÅÊÒÐÎÑÒÀÍÖÈÈ

73–77
(
5)

Êèñëîâ Î.Â.

FEATURES OF OPERATION MODE SELECTION OF CONVERTED GAS TURBINE ENGINE GAS GENERATORS

ÎÑÎÁËÈÂÎÑÒ² ÂÈÁÎÐÓ ÐÅÆÈÌÓ ÐÎÁÎÒÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÊÎÍÂÅÐÒÎÂÀÍÎÃÎ ÃÒÄ

ÎÑÎÁÅÍÍÎÑÒÈ ÂÛÁÎÐÀ ÐÅÆÈÌÀ ÐÀÁÎÒÛ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÊÎÍÂÅÐÒÈÐÎÂÀÍÍÎÃÎ ÃÒÄ

78–81
(
4)

Øêàáóðà Â.À.

ANALYSIS OF TURBO-COMPRESSOR WITH GENERAL IMPELLER FOR GAS TURBINE ENGINES

ÄÎÑË²ÄÆÅÍÍß ÒÓÐÁÎÊÎÌÏÐÅÑÎв ²Ç ÑϲËÜÍÈÌ ÐÎÁÎ×ÈÌ ÊÎËÅÑÎÌ ÄËß ÇÀÑÒÎÑÓÂÀÍÍß Ó ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓÍÀÕ

ÈÑÑËÅÄÎÂÀÍÈÅ ÒÓÐÁÎÊÎÌÏÐÅÑÑÎÐÎÂ Ñ ÎÁÙÈÌ ÐÀÁÎ×ÈÌ ÊÎËÅÑÎÌ ÏÐÈÌÅÍÈÒÅËÜÍÎ Ê ÃÀÇÎÒÓÐÁÈÍÍÛÌ ÄÂÈÃÀÒÅËßÌ

82–85
(
4)

Ëóêàøåâ È.Í.,
Ãîðáåíêî Ã.À.,
Ãàêàë Ï.Ã.,
×àéêà Ä.Â.,
Òóðíà Ð.Þ.

EXPERIMENAL RESEACH OF PROCESS IN THE VAPOR COMPRESSION REFRIGERATION PLANT WITH A SOLENOID VALVE AS A REGULATOR OF THE REFRIGERANT FLOW

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÏÐÎÖÅÑ²Â Ó ÏÀÐÎÊÎÌÏÐÅÑÎÐÍ²É ÕÎËÎÄÈËÜÍ²É ÌÀØÈͲ Ç ÑÎËÅÍίÄÍÈÌ ÊËÀÏÀÍÎÌ Ó ßÊÎÑÒ² ÐÅÃÓËßÒÎÐÀ ÂÈÒÐÀÒÈ ÕÎËÎÄÎÀÃÅÍÒÓ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÏÐÎÖÅÑÑΠ ÏÀÐÎÊÎÌÏÐÅÑÑÈÎÍÍÎÉ ÕÎËÎÄÈËÜÍÎÉ ÌÀØÈÍÅ Ñ ÑÎËÅÍÎÈÄÍÛÌ ÊËÀÏÀÍÎÌ Â ÊÀ×ÅÑÒÂÅ ÐÅÃÓËßÒÎÐÀ ÐÀÑÕÎÄÀ ÕËÀÄÀÃÅÍÒÀ

86–90
(
5)

Ðåìèçîâ À.Å.,
Êàðåëèí Î.Î.,
Ðåìèçîâ È.À.

to the question of choice of gasodynamic effectiveness parameter of  diffuser

ÄÎ ÏÈÒÀÍÍß âÈáîðÓ ïàðàìåòðÓ îö²íêè ãàçîäèíàì²÷Íί Åôåêòèâíîñò² äèôóçîðà

Ê ÂÎÏÐÎÑÓ ÂÛÁÎÐÀ ÏÀÐÀÌÅÒÐÀ ÎÖÅÍÊÈ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÄÈÔÔÓÇÎÐÀ

91–97
(
7)

Êîòêèí Â.Â.

MATHEMATICAL MODEL OF VISCOUS INTERACTION OF THE JETS AT THE GAS TURBINE ENGINE NOZZLE EXIT OF MULTI-MODE AIRCRAFT UNDER SUBSONIC EXTERNAL FLOW

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ Â'ßÇÊί ÂÇÀªÌÎIJ¯ ÑÒÐÓÌÅͲ ÍÀ ÂÈÕÎIJ ²Ç ÑÎÏËÀ ÃÒÄ ÁÀÃÀÒÎÐÅÆÈÌÍÎÃΠ˲ÒÀÊÀ  ÓÌÎÂÀÕ ÄÎÇÂÓÊÎÂÎÃÎ ÇÎÂͲØÍÜÎÃÎ ÎÁÒ²ÊÀÍÍß

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÂßÇÊÎÃÎ ÂÇÀÈÌÎÄÅÉÑÒÂÈß ÑÒÐÓÉ ÍÀ ÂÛÕÎÄÅ ÈÇ ÑÎÏËÀ ÃÒÄ ÌÍÎÃÎÐÅÆÈÌÍÎÃÎ ÑÀÌÎËÅÒÀ  ÓÑËÎÂÈßÕ ÄÎÇÂÓÊÎÂÎÃÎ ÂÍÅØÍÅÃÎ ÎÁÒÅÊÀÍÈß

98–102
(
5)

Ìàòâååâ Â.Í.,
Áàòóðèí Î.Â.,
Ïîïîâ Ã.Ì.

MULTISTAGE COMPRESSOR PERFORMANCES IMPROVEMENT BY USING OPTIMIZATION METHODS

ÏÎË²ÏØÅÍÍß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÁÀÃÀÒÎÑÒÓϲÍ×ÀÑÒÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÇÀ ÐÀÕÓÍÎÊ ÂÈÊÎÐÈÑÒÀÍÍß ÌÅÒÎIJ ÎÏÒÈ̲ÇÀÖ²¯

ÓËÓרÅÍÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÍÎÃÎÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÇÀ Ñ×¨Ò ÈÑÏÎËÜÇÎÂÀÍÈß ÌÅÒÎÄΠÎÏÒÈÌÈÇÀÖÈÈ

103–107
(
5)

Øåëêîâñêèé Ì.Þ.

AERODYNAMIC OPTIMIZATION METHOD OF COMPRESSOR BLADE VANES

ÌÅÒÎÄ ÀÅÐÎÄÈÍÀ̲×Íί ÎÏÒÈ̲ÇÀÖ²¯ ËÎÏÀÒÊÎÂÈÕ Â²Íֲ ÊÎÌÏÐÅÑÎÐÀ

ÌÅÒÎÄ ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÉ ÎÏÒÈÌÈÇÀÖÈÈ ËÎÏÀÒÎ×ÍÛÕ ÂÅÍÖΠÊÎÌÏÐÅÑÑÎÐÀ

108–115
(
8)

Ïåòåëü÷èö Â.Þ.,
Õàëàòîâ À.À.,
Ïèñüìåííûé Ä.Í.,
Äàøåâñêèé Þ.ß.

TO FILM COOLING RANS SIMULATION ACCURACY IMPROVING APPROACH

ÄÎ ÏÈÒÀÍÍß Ï²ÄÂÈÙÅÍÍß ÒÎ×ÍÎÑÒ² RANS ÌÎÄÅËÞÂÀÍÍß Ï˲ÂÊÎÂÎÃÎ ÎÕÎËÎÄÆÅÍÍß

Ê ÂÎÏÐÎÑÓ ÏÎÂÛØÅÍÈß ÒÎ×ÍÎÑÒÈ RANS ÌÎÄÅËÈÐÎÂÀÍÈß ÏËÅÍÎ×ÍÎÃÎ ÎÕËÀÆÄÅÍÈß

116–122
(
7)

Êîðîáêî Â.Â.

STUDY OF heat transfer and hydrodynamics in Components thermoacoustic ENGINES

Äîñë³äæåííÿ ïðîöåñ³â òåïëîîáì³íó òà ã³äðîäèíàì³êè â åëåìåíòàõ òåðìîàêóñòè÷íèõ äâèãóí³â

ÈÑÑËÅÄÎÂÀÍÈÅ ÏÐÎÖÅÑÑΠÒÅÏËÎÎÁÌÅÍÀ È ÃÈÄÐÎÄÈÍÀÌÈÊÈ Â ÝËÅÌÅÍÒÀÕ ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÈÕ ÄÂÈÃÀÒÅËÅÉ

123–130
(
8)

Ìàðêóøèí À.Í.,
Áàêëàíîâ À.Â.

HYDRAULIK CHARACTERISTICS OF SHORTENED MULTI-ATOMIZER COMBUSTOR OF GTE

òÄÐÀÂ˲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÓÊÎÐÎ×ÅÍί ÁÀÃÀÒÎÔÎÐÑÓÍÎ×Íί ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÂÌÄ

ÃÈÄÐÀÂËÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÓÊÎÐÎ×ÅÍÍÎÉ ÌÍÎÃÎÔÎÐÑÓÍÎ×ÍÎÉ ÊÀÌÅÐÛ ÑÃÎÐÀÍÈß ÃÒÄ

131–135
(
5)

Êðàâ÷åíêî È.Ô.,
Æóðàâëåâ Â.Í.,
Áîðçîâ Ñ.À.

RESEARCH THE IMPACT OF PRESSURE PULSATION IN COMBUSTION CHAMBER ON STABILITY WORK OF GAS TURBINE ENGINE

ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÏÀÐÀÌÅÒв ÏÓËÜÑÀÖ²É ÒÈÑÊÓ Ó ÊÀÌÅв ÇÃÎÐßÍÍß ÍÀ ÑÒ²ÉʲÑÒÜ ÐÎÁÎÒÈ ÃÒÄ

ÈÑÑËÅÄÎÂÀÍÈÅ ÂËÈßÍÈß ÏÀÐÀÌÅÒÐΠÏÓËÜÑÀÖÈÉ ÄÀÂËÅÍÈß Â ÊÀÌÅÐÅ ÑÃÎÐÀÍÈß ÍÀ ÓÑÒÎÉ×ÈÂÎÑÒÜ ÐÀÁÎÒÛ ÃÒÄ

136–141
(
6)

Êîðíèåíêî Â.Ñ.

RESEARCH OF SMALL PRODUCTIVITY ROTARY INJECTORS WORK

ÄÎÑË²ÄÆÅÍÍß ÐÎÁÎÒÈ ÐÎÒÀÖ²ÉÍÈÕ ÔÎÐÑÓÍÎÊ ÌÀËί ÏÐÎÄÓÊÒÈÂÍÎÑÒ²

ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÁÎÒÛ ÐÎÒÀÖÈÎÍÍÛÕ ÔÎÐÑÓÍÎÊ ÌÀËÎÉ ÏÐÎÈÇÂÎÄÈÒÅËÜÍÎÑÒÈ

142–146
(
5)

Ñåðáèí Ñ.È.,
Ãîí÷àðîâà Í.À.

THE NUMERICAL SIMULATION OF THE PLASMA COAL OXYGEN AND OXYGEN-STEAM GASIFICATION PROCESSES

×ÈÑÅËÜÍÅ ÌÎÄÅËÞÂÀÍÍß ÏÐÎÖÅѲ ÏËÀÇÌÎÂί ÊÈÑÍÅÂί ² ÊÈÑÍÅÂÎ-ÏÀÐÎÂί ÃÀÇÈÔÈÊÀÖ²¯ ÂÓòËËß

×ÈÑËÅÍÍÎÅ ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÖÅÑÑΠÏËÀÇÌÅÍÍÎÉ ÊÈÑËÎÐÎÄÍÎÉ È ÊÈÑËÎÐÎÄÍÎ-ÏÀÐÎÂÎÉ ÃÀÇÈÔÈÊÀÖÈÈ ÓÃËÅÉ

147–150
(
4)

Áîíäàðåíêî Ì.Ñ.,
×åïëþõà Ì.Î.

THE LNG-TERMINAL REGASIFICATION UNIT WITH GAS-TURBINE FOR ELECTRIC POWER GENERATION

ÃÒÓ Â ÑÊËÀIJ ÐÅÃÀÇÈÔ²ÊÀÖ²ÉÍÎÃÎ ÊÎÌÏËÅÊÑÓ LNG–ÒÅÐ̲ÍÀËÓ

ÃÒÓ Â ÑÎÑÒÀÂÅ ÐÅÃÀÇÈÔÈÊÀÖÈÎÍÍÎÃÎ ÊÎÌÏËÅÊÑÀ LNG–ÒÅÐÌÈÍÀËÀ

151–154
(
4)

Ùóêèí Â.À.,
Âàëèåâ Ô.Ì.,
Äóíàé Î.Â
.

PARTICULARITIES OF THE FORMATION TOXIC SUBSTANCES IN TURBULENT DIFFUZION COMBUSTION GAS

ÎÑÎÁËÈÂÎÑÒ² ÓÒÂÎÐÅÍÍß ÒÎÊÑÈ×ÍÈÕ ÐÅ×ÎÂÈÍ ÏÐÈ ÒÓÐÁÓËÅÍÒÍÎÌÓ ÄÈÔÓDzÉÍÎÌÓ ÇÃÎÐßÍͲ ÃÀDzÂ

ÎÑÎÁÅÍÍÎÑÒÈ ÎÁÐÀÇÎÂÀÍÈß ÒÎÊÑÈ×ÍÛÕ ÂÅÙÅÑÒ ÏÐÈ ÒÓÐÁÓËÅÍÒÍÎÌ ÄÈÔÔÓÇÈÎÍÍÎÌ ÃÎÐÅÍÈÈ ÃÀÇÎÂ

155–159
(
5)

Íàçèí Â.È.

THEORY OF DOUBLE RADIAL BEARING IN GIDROSTATODINAMICHESKOGO STATIONARY EXTERNAL LOAD

ÒÅÎÐ²ß ÇÄÂΪÍÍß ÐÀIJÀËÜÍÎÃΠòÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÏÐÈ ÍÅÑÒÀÖ²ÎÍÀÐÍÎÌÓ ÇÎÂͲØÍÜÎÌÓ ÍÀÂÀÍÒÀÆÅÍͲ

ÒÅÎÐÈß ÑÄÂÎÅÍÍÎÃÎ ÐÀÄÈÀËÜÍÎÃÎ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÏÐÈ ÍÅÑÒÀÖÈÎÍÀÐÍÎÉ ÂÍÅØÍÅÉ ÍÀÃÐÓÇÊÅ

160–166
(
7)

Äîëìàòîâ Ä.À.

HYDROXYL AND ATOMIC OXYGEN GENERATION BY SMALL PLASMA INCLUSIONS

ÃÅÍÅÐÀÖ²ß Ã²ÄÐÎÊÑÈ˲ ÒÀ ÀÒÎÌÀÐÍÎÃÎ ÊÈÑÍÞ ÏÎÁËÈÇÓ ÌÀËÈÕ ÏËÀÇÌÎÂÈÕ ÂÊËÞ×ÅÍÜ

ÃÅÍÅÐÀÖÈß ÃÈÄÐÎÊÑÈËÎÂ È ÀÒÎÌÀÐÍÎÃÎ ÊÈÑËÎÐÎÄÀ ÂÁËÈÇÈ ÌÀËÛÕ ÏËÀÇÌÅÍÍÛÕ ÂÊËÞ×ÅÍÈÉ

167–171
(
5)

Âèíîãðàäîâ À.Ñ.,
Øïàêîâ È.Ä.,
Ãîðÿ÷êèí Å.Ñ.

ANALYSIS OF RADIAL FACE CONTACT SEAL efficiency IN THE SUPPORT OF THE AIRCRAFT ENGINE COMPRESSOR AT VARIOUS OPERATIONAL MODES

ÀÍÀË²Ç ÏÐÀÖÅÇÄÀÒÍÎÑÒ² ̲ÆÂÀËÜÍÎÃΠ ÐÀIJÀËÜÍÎ-òîðöåâÎÃÎ ÊÎÍÒÀÊÒÍÎÃÎ ÓÙ²ËÜÍÅÍÍß

ÀÍÀËÈÇ ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÈ ÌÅÆÂÀËÜÍÎÃÎ ÐÀÄÈÀËÜÍÎ-ÒÎÐÖÅÂÎÃÎ ÊÎÍÒÀÊÒÍÎÃÎ ÓÏËÎÒÍÅÍÈß

172–175
(
4)

Òèñàðåâ À.Þ.,
Âàñèëåâè÷ Í.Ì.

Investigation of labirint sealS perfoRmanCes with deformations of sealing surfaces

ÄÎÑË²ÄÆÅÍÍß ÂÈÒÐÀÒÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ Ëàá³ðèíòîâîãî óù³ëüíåííÿ Ç ÓÐÀÕÓÂÀÍÍßÌ ÄÅÔÎÐÌÀÖ²É ÓÙ²ËÜÍÞÂÀËÜÍÈÕ ÏÎÂÅÐÕÎÍÜ

ÈÑÑËÅÄÎÂÀÍÈÅ ÐÀÑÕÎÄÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ËÀÁÈÐÈÍÒÍÛÕ ÓÏËÎÒÍÅÍÈÉ Ñ ÓרÒÎÌ ÄÅÔÎÐÌÀÖÈÉ ÓÏËÎÒÍÈÒÅËÜÍÛÕ ÏÎÂÅÐÕÍÎÑÒÅÉ

176–180
(
5)

Íîâèêîâ Ä.Ê.,
Äèëèãåíñêèé Ä.Ñ.

DEVELOPMENT OF MODEL OF SQUEEZE-FILM DAMPER WITH METERING GROOVES

ÐÎÇÐÎÁÊÀ ÌÎÄÅ˲ òÄÐÎÄÈÍÀ̲×ÍÎÃÎ äåìïôåðà Ç ÄÐÎÑÅËÞÞ×ÈÌÈ êàíàâêàìè

ÐÀÇÐÀÁÎÒÊÀ ÌÎÄÅËÈ ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÄÅÌÏÔÅÐÀ Ñ ÄÐÎÑÑÅËÈÐÓÙÈÌÈ ÊÀÍÀÂÊÀÌÈ

181–184
(
4)

Ñû÷åâà Í.Ñ.,
Ðîäþê Ñ.À.

NEW APPROACH FOR DESIGNING AND TESTING AN OIL TANK OF A HIGHLY MANUVERING AIR VEHICLE ENGINE

ÌÅÒÎÄI×ÍÈÉ ÏIÄÕIÄ ÄÎ ÏÐÎÅÊÒÓÂÀÍÍß ÒÀ ÂÈÏÐÎÁÓÂÀÍÜ ÌÀÑËßÍÎÃÎ ÁÀÊÀ ÄËß ÄÂÈÃÓÍÀ ÌÀÍÅÂÐÅÍÎÃÎ ËIÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ

ÌÅÒÎÄÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÏÐÎÅÊÒÈÐÎÂÀÍÈÞ È ÈÑÏÛÒÀÍÈßÌ ÌÀÑËÎÁÀÊÀ ÄËß ÄÂÈÃÀÒÅËß ÌÀÍÅÂÐÅÍÍÎÃÎ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ

185–188
(
4)

Ìîãèëüíèêîâ Â.Ï.,
Èîíîâ À.Â.

EQUIPMENT FOR AIR SAMPLING FROM ENGINE

ÀÏÀÐÀÒͲ ÇÀÑÎÁÈ ÄËß Â²ÄÁÈÐÀÍÍß ÏÐÎÁ ÏβÒÐß À²ÀÖ²ÉÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲÂ

ÀÏÏÀÐÀÒÍÛÅ ÑÐÅÄÑÒÂÀ ÄËß ÎÒÁÎÐÀ ÏÐÎÁ ÂÎÇÄÓÕÀ ÀÂÈÀÖÈÎÍÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

189–196
(
8)

Îñàä÷èé Í.Â.,
Ñåðãååâ À.À.,
Øåïåëü Â.Ò.

THE ASSURANCE OF CERTIFICATION REQUIREMENTS SHOWN TO THE TURBOFAN ENGINE FAN CASE

ÇÀÁÅÇÏÅ×ÅÍÍß ÑÅÐÒÈÔ²ÊÀÖ²ÉÍÈÕ âèìîã, ùî ïðåä'ÿâëÿþòüñÿ Äî êîðïóñó âåíòèëÿòîðà ÒÐÄÄ

ÎÁÅÑÏÅ×ÅÍÈÅ ÑÅÐÒÈÔÈÊÀÖÈÎÍÍÛÕ ÒÐÅÁÎÂÀÍÈÉ, ÏÐÅÄÚßÂËßÅÌÛÕ Ê ÊÎÐÏÓÑÓ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ

197–200
(
4)

Ïàðîâàé Å.Ô.,
Ïàðîâàé Ô.Â.

Hydrodynamic bearing with MR elastic suspension of segments

òÄÐÎÄÈÍÀ̲×ÍÈÉ Ï²ÄØÈÏÍÈÊ ç ïðóæíèìè ï³äâ³ñîì âêëàäèø³â ç ÌÀÒÅвÀËÓ ÌÐ

ÃÈÄÐÎÄÈÍÀÌÈ×ÅÑÊÈÉ ÏÎÄØÈÏÍÈÊ Ñ ÓÏÐÓÃÈÌ ÏÎÄÂÅÑÎÌ ÂÊËÀÄÛØÅÉ ÈÇ ÌÀÒÅÐÈÀËÀ ÌÐ

201–205
(
5)

Ëîÿí À.Â.,
Òèòîâ Ì.Þ.,
Ñîëîíèíêî Å.Ï.

ELECTRIC FIELD HETEROGENEITY MINIMIZATION DURING TESTS OF EMITTERS IN ELECTRIC PROPULSION CATHODES

̲Ͳ̲ÇÀÖ²ß ÍÅÎÄÍÎвÄÍÎÑÒ² ÅËÅÊÒÐÈ×ÍÎÃÎ ÏÎËß ÏÐÈ ÂÈÏÐÎÁÓÂÀÍÍßÕ Å̲ÒÅв ÊÀÒÎIJ ÅÐÄ

ÌÈÍÈÌÈÇÀÖÈß ÍÅÎÄÍÎÐÎÄÍÎÑÒÈ ÝËÅÊÒÐÈ×ÅÑÊÎÃÎ ÏÎËß ÏÐÈ ÈÑÏÛÒÀÍÈßÕ ÝÌÈÒÒÅÐΠÊÀÒÎÄΠÝÐÄ

206–210
(
5)

Ôåäîð÷åíêî Ä.Ã.,
Ãëàäêîâ À.Â.,
Ñîëÿííèêîâ Â.À.,
Æóæóêèí À.È.

SPECKLE-INTERFEROMETER FOR GAS TURBINE ENGINE LARGE-SIZE PARTS AND COMPONENTS VIBRATIONS STUDY

ÑÏÅÊË-²ÍÒÅÐÔÅÐÎÌÅÒÐ ÄËß ÄÎÑË²ÄÆÅÍÍß ÊÎËÈÂÀÍÜ ÂÅËÈÊÎÃÀÁÀÐÈÒÍÈÕ ÄÅÒÀËÅÉ ² ÂÓÇ˲ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲÂ

ÑÏÅÊË – ÈÍÒÅÐÔÅÐÎÌÅÒÐ ÄËß ÈÑÑËÅÄÎÂÀÍÈß ÊÎËÅÁÀÍÈÉ ÊÐÓÏÍÎÃÀÁÀÐÈÒÍÛÕ ÄÅÒÀËÅÉ È ÓÇËÎÂ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

211–215
(
5)

Ðÿáêîâ Â.È.,
Òîëìà÷åâ Í.Ã.

HAVE THE HIGGS BOSON BEEN DISCOVERED

×È Â²ÄÊÐÈÒÈÉ ÁÎÇÎÍ Õ²ÃÑÀ?

ÎÒÊÐÛÒ ËÈ ÁÎÇÎÍ ÕÈÃÃÑÀ?

216–221
(
6)

Èíôîðìàöèîííûå òåõíîëîãèè

Êóëèêîâ Ã.Ã.,
Ôàòèêîâ Â.Ñ.,
Òðóøèí Â.À.,
Ãàíååâ À.À.,
Àáäóëíàãèìîâ À.È.

MONITORING CONCEPT OF THERMAL STRESS STATE AND BLADE RESOURCE FOR HEAVY-DUTY GAS TURBINES

ÊÎÍÖÅÏÖ²ß ÌÎͲÒÎÐÈÍÃÓ ÒÅÐÌÎÍÀÏÐÓÆÅÍÎÃÎ ÑÒÀÍÓ ² ÐÅÑÓÐÑÓ ËÎÏÀÒÎÊ ÂÈÑÎÊÎÍÀÂÀÍÒÀÆÅÍÈÕ ÒÓÐÁ²Í À²ÀÖ²ÉÍÈÕ ÃÒÄ

ÊÎÍÖÅÏÖÈß ÌÎÍÈÒÎÐÈÍÃÀ ÒÅÐÌÎÍÀÏÐ߯ÅÍÍÎÃÎ ÑÎÑÒÎßÍÈß È ÐÅÑÓÐÑÀ ËÎÏÀÒÎÊ ÂÛÑÎÊÎÍÀÃÐÓÆÅÍÍÛÕ ÒÓÐÁÈÍ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

222–228
(
7)

Goncharenko A.V.

SUBJECTIVE ENTROPY EXTREMIZATION PRINCIPLE AS A TOOL OF AN AIRCRAFT MAXIMAL DURATION HORIZONTAL FLIGHT CONTROL

ÏÐÈÍÖÈÏ ÅÊÑÒÐÅ̲ÇÀÖ²¯ ÑÓÁ’ªÊÒÈÂÍί ÅÍÒÐÎϲ¯ ßÊ ²ÍÑÒÐÓÌÅÍÒ ÊÅÐÓÂÀÍÍß ÌÀÊÑÈÌÀËÜÍÎÞ ÒÐÈÂÀ˲ÑÒÞ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÜÎÒÓ Ë²ÒÀÊÀ

ÏÐÈÍÖÈÏ ÝÊÑÒÐÅÌÈÇÀÖÈÈ ÑÓÁÚÅÊÒÈÂÍÎÉ ÝÍÒÐÎÏÈÈ ÊÀÊ ÈÍÑÒÐÓÌÅÍÒ ÓÏÐÀÂËÅÍÈß ÌÀÊÑÈÌÀËÜÍÎÉ ÏÐÎÄÎËÆÈÒÅËÜÍÎÑÒÜÞ ÃÎÐÈÇÎÍÒÀËÜÍÎÃÎ ÏÎËÅÒÀ ÑÀÌÎËÅÒÀ

229–234
(6)

Ïàí³í Â.Â.,
ªí÷åâ Ñ.Â.,
Òîâêà÷ Ñ.Ñ.

COMBINED MODELS OF INFORMATION PROCESSING IN THE ELECTRONIC CONTROL SYSTEMS OF AIRCRAFT ENGINES

ÊÎÌÁ²ÍÎÂÀͲ ÌÎÄÅ˲ ÎÁÐÎÁÊÈ ²ÍÔÎÐÌÀÖ²¯  ÅËÅÊÒÐÎÍÍÈÕ ÑÈÑÒÅÌÀÕ ÊÅÐÓÂÀÍÍß À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÊÎÌÁÈÍÈÐÎÂÀÍÍÛÅ ÌÎÄÅËÈ ÎÁÐÀÁÎÒÊÈ ÈÍÔÎÐÌÀÖÈÈ Â ÝËÅÊÒÐÎÍÍÛÕ ÑÈÑÒÅÌÀÕ ÓÏÐÀÂËÅÍÈß ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

235–239
(
5)

Áóðÿ÷åíêî À.Ã.,
Ðàí÷åíêî Ã.Ñ.,
Ðÿáîêîíü Ñ.Ì.

PARAMETRIC RELIABILITY RESEARCH RESULTS OF AIRCRAFT PRESSURE TRANSDUCERS

ÐÅÇÓËÜÒÀÒÈ ÄÎÑËIÄÆÅÍÍß ÏÀÐÀÌÅÒÐÈ×Íί ÍÀÄIÉÍÎÑÒ² ÀÂÈÀÖIÉÍÈÕ ÄÀÒ×ÈÊI ÒÈÑÊÓ

ÐÅÇÓËÜÒÀÒÛ ÈÑÑËÅÄÎÂÀÍÈß ÏÀÐÀÌÅÒÐÈ×ÅÑÊÎÉ ÍÀÄÅÆÍÎÑÒÈ ÀÂÈÀÖÈÎÍÍÛÕ ÄÀÒ×ÈÊΠÄÀÂËÅÍÈß

240–245
(
6)

Ìèðãîðîä Â.Ô.,
Äåðåíã Å.Â.

CLUSTERS EXTRACTION AT MULTIDIMENSIONAL TREND ANALYSIS

ÂÈIJËÅÍÍß ÊËÀÑÒÅв ÏÐÈ ÁÀÃÀÒÎÂÈ̲ÐÍÎÌÓ ÒÐÅÍÄÎÂÎÌ ÀÍÀ˲Dz

ÂÛÄÅËÅÍÈÅ ÊËÀÑÒÅÐÎÂ ÏÐÈ ÌÍÎÃÎÌÅÐÍÎÌ ÒÐÅÍÄÎÂÎÌ ÀÍÀËÈÇÅ

246–249
(
4)

Äàâèäåíêî Â.Î.

METHOD OF COMPUTER MONITORING OF THE ZONE OF CHEMICAL POLLUTION IN CASE OF EMERGENCY EMISSIONS OF POISONING CHEMICALS IN THE ATMOSPHERE

ÌÅÒÎÄ ÊÎÌÏ'ÞÒÅÐÍÎÃÎ ÌÎͲÒÎÐÈÍÃÓ ÇÎÍÈ Õ²Ì²×ÍÎÃÎ ÇÀÁÐÓÄÍÅÍÍß ÏÐÈ ÀÂÀвÉÍÈÕ ÂÈÊÈÄÀÕ ÎÒÐÓÉËÈÂÈÕ Õ²Ì²×ÍÈÕ ÐÅ×ÎÂÈÍ Â ÀÒÌÎÑÔÅÐÓ

ÌÅÒÎÄ ÊÎÌÏÜÞÒÅÐÍÎÃÎ ÌÎÍÈÒÎÐÈÍÃÀ ÇÎÍÛ ÕÈÌÈ×ÅÑÊÎÃÎ ÇÀÃÐßÇÍÅÍÈß ÏÐÈ ÀÂÀÐÈÉÍÛÕ ÂÛÁÐÎÑÀÕ ÎÒÐÀÂËßÞÙÈÕ ÕÈÌÈ×ÅÑÊÈÕ ÂÅÙÅÑÒ  ÀÒÌÎÑÔÅÐÓ

250–254
(
5)

Òðåòüÿê Â.Â.,
Ìàòóñåâè÷ Í.Ñ.,
Íåâåøêèí Þ.À, Îíîï÷åíêî À.Â.,
Ãîëîâàíîâà Ì.À
.

DEVELOPMENT OF INFORMATION AND MATHEMATICAL MODEL FOR CALCULATING THE ECONOMIC EFFICIENCY CAD PULSED PROCESSES

ÐÎÇÐÎÁÊÀ ÌÀÒÅÌÀÒÈ×Íί ÒÀ ²ÍÔÎÐÌÀÖ²ÉÍί ÌÎÄÅ˲ ÄËß ÐÎÇÐÀÕÓÍÊÓ ÅÊÎÍÎ̲×Íί ÅÔÅÊÒÈÂÍÎÑÒ² ÂÈÊÎÐÈÑÒÀÍÍß ÑÀÏÐ ²ÌÏÓËÜÑÍÈÕ ÏÐÎÖÅѲÂ

ÐÀÇÐÀÁÎÒÊÀ ÌÀÒÅÌÀÒÈ×ÅÑÊÎÉ È ÈÍÔÎÐÌÀÖÈÎÍÍÎÉ ÌÎÄÅËÈ ÄËß ÐÀÑ×ÅÒÀ ÝÊÎÍÎÌÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÈÑÏÎËÜÇÎÂÀÍÈß ÑÀÏÐ ÈÌÏÓËÜÑÍÛÕ ÏÐÎÖÅÑÑÎÂ

255–259
(
5)

Êó÷óê Ã.À.

MODELLING OF THE WIRELESS NETWORK AGGREGATED TRAFFIC ON THE BASIS OF INFORMATIVE STREAMS STATISTICAL MONITORING

ÌÎÄÅËÞÂÀÍÍß ÀÃÐÅÃÎÂÀÍÎÃÎ ÒÐÀÔ²ÊÀ ÁÅÇÏÐβÄÍί ÌÅÐÅÆ² ÏÅÐÅÄÀײ ÄÀÍÈÕ, ÙÎ ¥ÐÓÍÒÓªÒÜÑß ÍÀ ÑÒÀÒÈÑÒÈ×ÍÎÌÓ ÌÎͲÒÎÐÈÍDz ²ÍÔÎÐÌÀÖ²ÉÍÈÕ ÏÎÒÎʲÂ

ìîäåëèðîâàíèÅ àãðåãèðîâàííîãî òðàôèêà áåñïðîâîäíîé ñåòè ïåðåäà÷è äàííûõ íà Îñíîâå ñòàòèñòè÷åñêîãî ìîíèòîðèíãà èíôîðìàöèîííûõ ïîòîêîâ

260–264
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5)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Íåñòåðåíêî Â.Ã.,
Ñèðîòèí Í.Í.,
Àãóëüíèê À.Á.,
Ðàâèêîâè÷ Þ.À.

COMPREHENSIVE TRAINING OF UNIVERSITY STUDENTS IN «AIRCRAFT ENGINES AND POWER PLANTS»

ÊÎÌÏËÅÊÑÍÀ ϲÄÃÎÒÎÂÊÀ Ó×Ͳ ÂÈÙÈÕ ÍÀÂ×ÀËÜÍÈÕ ÇÀÊËÀIJ  ÇÀ ÑÏÅÖ²ÀËÜͲÑÒÞ «À²ÀÖ²ÉͲ ÄÂÈÃÓÍÈ ² ÅÍÅÐÃÅÒÈ×Ͳ ÓÑÒÀÍÎÂÊÈ»

ÊÎÌÏËÅÊÑÍÀß ÏÎÄÃÎÒÎÂÊÀ Ó×ÀÙÈÕÑß ÂÛÑØÈÕ Ó×ÅÁÍÛÕ ÇÀÂÅÄÅÍÈÉ ÏÎ ÑÏÅÖÈÀËÜÍÎÑÒÈ «ÀÂÈÀÖÈÎÍÍÛÅ ÄÂÈÃÀÒÅËÈ È ÝÍÅÐÃÅÒÈ×ÅÑÊÈÅ ÓÑÒÀÍÎÂÊÈ»

265–268
(
4)

Ñòåïàíåíêî Ñ.Ì.,
Òåâñ À.À.,
Õàð÷åíêî Â.Ã.

ESTIMATION OF QUALITY MANAGEMENT SYSTEMS PROCESSS EFFECTIVENESS OF COMPANIES INVOLVED IN DESIGN OF AVIATION PRODUCTS

ÎÖ²ÍÊÀ ÐÅÇÓËÜÒÀÒÈÂÍÎÑÒ² ÏÐÎÖÅѲ ÑÈÑÒÅÌ ÌÅÍÅÄÆÌÅÍÒÓ ßÊÎÑÒ² ϲÄÏÐȪÌÑÒ ÐÎÇÐÎÁÍÈʲ À²ÀÖ²ÉÍί ÒÅÕͲÊÈ

ÎÖÅÍÊÀ ÐÅÇÓËÜÒÀÒÈÂÍÎÑÒÈ ÏÐÎÖÅÑÑΠÑÈÑÒÅÌ ÌÅÍÅÄÆÌÅÍÒÀ ÊÀ×ÅÑÒÂÀ ÏÐÅÄÏÐÈßÒÈÉ ÐÀÇÐÀÁÎÒ×ÈÊΠÀÂÈÀÖÈÎÍÍÎÉ ÒÅÕÍÈÊÈ

269–272
(
4)

Ðåâà Î.Ì.,
̳ðçîºâ Á.Ì.,
Ìóõòàðîâ Ï.Ø.,
Íàñ³ðîâ Ø.Ø.

LEVEL OF CLAIMS OF AIR TRAFFIC CONTROLLERS FOR RESULTS OF WORKING LOAD

вÂÅÍÜ ÄÎÌÀÃÀÍÜ À²ÀÄÈÑÏÅÒ×Åв ÍÀ ÏÎÊÀÇÍÈÊÀÕ ÐÎÁÎ×ÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß

ÓÐÎÂÅÍÜ ÏÐÈÒßÇÀÍÈÉ ÀÂÈÀÄÈÑÏÅÒ×ÅÐΠÍÀ ÏÎÊÀÇÀÒÅËßÕ ÐÀÁÎ×ÅÉ ÍÀÃÐÓÇÊÈ

273–281
(
9)

Äàíîâà Ì.À.

SYNTHESIS MODEL SELECTION OF PRIORITIES FOR PREDICTING THE SCIENTIFIC AND TECHNICAL DEVELOPMENT USING TECHNOLOGY FORESIGHT

ÑÈÍÒÅÇ ÌÎÄÅ˲ ÂÈÁÎÐÓ ÏвÎÐÈÒÅҲ ÏÐÈ ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÈ ÍÀÓÊÎÂÎ-ÒÅÕͲ×ÍÎÃÎ ÐÎÇÂÈÒÊÓ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÒÅÕÍÎËÎò¯ ÔÎÐÑÀÉÒ

ÑÈÍÒÅÇ ÌÎÄÅËÈ ÂÛÁÎÐÀ ÏÐÈÎÐÈÒÅÒΠÏÐÈ ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÈ ÍÀÓ×ÍÎ-ÒÅÕÍÈ×ÅÑÊÎÃÎ ÐÀÇÂÈÒÈß Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÒÅÕÍÎËÎÃÈÈ ÔÎÐÑÀÉÒ

282–286
(
5)

Äåìüÿíåíêî Â.À.

INFORMATION SUPPORT OF PRODUCTION OF CONSUMER GOODS AT MULTIPRODUCT MACHINE-BUILDING ENTERPRISE

²ÍÔÎÐÌÀÖ²ÉÍÀ ϲÄÒÐÈÌÊÀ ÂÈÐÎÁÍÈÖÒÂÀ ÒÎÂÀв ÍÀÐÎÄÍÎÃÎ ÑÏÎÆÈÂÀÍÍß ÍÀ ÁÀÃÀÒÎÍÎÌÅÍÊËÀÒÓÐÍÎÌÓ ÌÀØÈÍÎÁÓIJÂÍÎÌÓ Ï²ÄÏÐȪÌÑÒ²

ÈÍÔÎÐÌÀÖÈÎÍÍÀß ÏÎÄÄÅÐÆÊÀ ÏÐÎÈÇÂÎÄÑÒÂÀ ÒÎÂÀÐÎÂ ÍÀÐÎÄÍÎÃÎ ÏÎÒÐÅÁËÅÍÈß ÍÀ ÌÍÎÃÎÍÎÌÅÍÊËÀÒÓÐÍÎÌ ÌÀØÈÍÎÑÒÐÎÈÒÅËÜÍÎÌ ÏÐÅÄÏÐÈßÒÈÈ

287–292
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5)

 

 

 

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 íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.