Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2014. – ¹ 9
(116). – 188 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2014. – ¹ 9 (116). –
188 ñ.
ISSN
1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2014. – ¹ 9 (116). – 188 ñ.
Ìàòåðèàëû, ñîäåðæàùèåñÿ â æóðíàëå,
îïóáëèêîâàíû
ïî ðåøåíèþ XIX ìåæäóíàðîäíîãî êîíãðåññà äâèãàòåëåñòðîèòåëåé
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè (article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Øóëüæåíêî Í. Ã., |
Numerical simulation of dynamic response of structure under impulse
impact |
×ÈÑÅËÜÍÅ ÌÎÄÅËÞÂÀÍÍß ÄÈÍÀ̲×Íί ÐÅÀÊÖ²¯
ÊÎÍÑÒÐÓÊÖ²É ÍÀ ²ÌÏÓËÜÑÍÈÉ ÂÏËÈ |
×ÈÑËÅÍÍÎÅ
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÄÈÍÀÌÈ×ÅÑÊÎÉ ÐÅÀÊÖÈÈ ÊÎÍÑÒÐÓÊÖÈÉ ÍÀ ÈÌÏÓËÜÑÍÎÅ ÂÎÇÄÅÉÑÒÂÈÅ |
6–11 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Òåðåøèí À. Ì., |
RESEARCHES AIR
INLETS OF HIGH-SPEED RAMJET |
ÄÎÑË²ÄÆÅÍÍß
ÏβÒÐÎÇÀÁ²ÐÍÈÕ ÏÐÈÑÒÐί ÂÈÑÎÊÎØÂÈÄʲÑÍÈÕ ÏÏÐÄ |
ÈÑÑËÅÄÎÂÀÍÈß
ÂÎÇÄÓÕÎÇÀÁÎÐÍÛÕ ÓÑÒÐÎÉÑÒÂ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÛÕ ÏÂÐÄ |
12–16 |
Ãðåöêîâ À. È., |
AERODYNAMIC
CHARACTERISTICS ESTIMATION OF HELICOPTER IN THE PROBLEM OF SELECTION
PARAMETER VALUES OF WORK GAS TURBINE ENGINE WITH A FREE TURBINE |
ÄÎ ÎÖ²ÍÊÈ ÀÅÐÎÄÈÍÀÌI×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÂÅÐÒÎËÜÎÒÀ  ÇÀÄÀײ ÂÈÁÎÐÓ ÇÍÀ×ÅÍÜ ÏÀÐÀÌÅÒв ÐÎÁÎ×ÎÃÎ ÏÐÎÖÅÑÓ ÃÒÄ ÂÒ |
17–20 |
|
Êóõòèí Þ. Ï., |
CONJUGATED NUMERICAL MODELING OF INTERNAL AND EXTERNAL AERODYNAMICS OF
ENGINE-AIRFRAME SYSTEM |
CÏÐ߯ÅÍÅ ÷èñÅËÜÍÅ ìîäåëþâàííÿ ÂÍÓÒвØÍÜο ² ÇÎÂͲØÍÜί àåðîäèíàì³êè ÑÈÑÒÅÌÈ
ÄÂÈÃÓÍ - ÊÎÐÏÓÑ Ë²ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ |
21–26 |
|
Øåëêîâñêèé Ì. Þ. |
AERODYNAMIC IMPROVEMENT OF AXIAL
TEN-STAGE COMPRESSOR OF STATIONARY GTE |
ÀÅÐÎÄÈÍÀ̲×ÍÅ ÂÄÎÑÊÎÍÀËÅÍÍß
ÎÑÜÎÂÎÃÎ ÄÅÑßÒÈÑÒÓϲÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÎÐÀ ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÃÒÄ |
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÎÅ
ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÎÑÅÂÎÃÎ ÄÅÑßÒÈÑÒÓÏÅÍ×ÀÒÎÃÎ ÊÎÌÏÐÅÑÑÎÐÀ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÃÒÄ |
27–32 |
Äîëìàòîâ Ä. À., |
THE INTERACTION
OF POOR FLAMES WITH DIFFERENT TEMPERATURES |
ÂÇÀªÌÎÄ²ß Á²ÄÍÈÕ ÃÅÒÅÐÎÃÅÍÍÈÕ ÏÎËÓÌ’¯Â
Ç Ð²ÇÍÎÞ ÒÅÌÏÅÐÀÒÓÐÎÞ |
ÂÇÀÈÌÎÄÅÉÑÒÂÈÅ
ÁÅÄÍÛÕ ÃÅÒÅÐÎÃÅÍÍÛÕ ÏËÀÌÅÍ Ñ ÐÀÇËÈ×ÍÎÉ ÒÅÌÏÅÐÀÒÓÐÎÉ |
33–38 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Òêà÷ Ì. Ð., |
EFFICIENCY OF HEAT RECOVERY BY METAL-HYDRIDE INSTALLATION
OF CONTINUOUS OPERATION |
ÅÔÅÊÒÈÂͲÑÒÜ ÓÒÈ˲ÇÀÖ²¯ ÒÅÏËÀ
ÌÅÒÀËÎòÄÐÈÄÍί ÓÑÒÀÍÎÂÊÈ ÁÅÇÏÅÐÅÐÂÍί IJ¯ |
39–44 |
|
Áåëîóñîâ Å. Â. |
WASTE SEPARATION FUEL USING ENERGY BALANCE SHIP
POWER PLANTS |
ÂÈÊÎÐÈÑÒÀÍÍß Â²ÄÕÎIJ ÑÅÏÀÐÀÖ²¯ ÏÀËÈÂÀ
 ÏÀËÈÂÍÎÌÓ ÁÀËÀÍѲ ÑÓÄÍÎÂί ÅÍÅÐÃÅÒÈ×Íί ÓÑÒÀÍÎÂÊÈ |
ÈÑÏÎËÜÇÎÂÀÍÈÅ
ÎÒÕÎÄΠÑÅÏÀÐÀÖÈÈ ÒÎÏËÈÂÀ  ÒÎÏËÈÂÍÎÌ ÁÀËÀÍÑÅ ÑÓÄÎÂÎÉ ÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ
ÓÑÒÀÍÎÂÊÈ |
45–49 |
Ëèñèöà À. Þ., |
ON EFFICIENCY OF INDIRECT EVAPORATIVE COOLING FOR GTU CYCLIC AIR |
ÄÎ ÏÈÒÀÍÍß ªÔÅÊÒÈÂÍÎÑÒ² ÍÅÏÐßÌÎÃÎ
ÂÈÏÀÐÍÎÃÎ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÃÒÏ |
Ê ÂÎÏÐÎÑÓ
ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÎÑÂÅÍÍÎ-ÈÑÏÀÐÈÒÅËÜÍÎÃÎ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÃÒÏ |
50–55 |
Ìàìåäîâ Á. Ø. |
ÒÍÅ SINGLE THEORY
OF CONTINUOS FLOW PROPULSION. THE REASONS OF TURBO-JET UNSTEADY WORK
GENERATION WHILE TAKE OFF IN CONDITIONS OF HOT CLIMATE |
ªÄÈÍÀ ÒÅÎÐ²ß ÐÓØ²¯Â. ÏÐÈ×ÈÍÈ
ÃÅÍÅÐÓÂÀÍÍß ÍÅÑÒ²ÉÊί ÐÎÁÎÒÈ ÒÓÐÁÎÐÅÀÊÒÈÂÍÈÕ ÄÂÈÃÓͲ ÏÐÈ ÇËÜÎÒ²  ÓÌÎÂÀÕ
ÑÏÅÊÎÒÍÎÃÎ Ê˲ÌÀÒÓ |
56–62 |
|
Øêàáóðà Â. À. |
RESULTS OF ANALYSIS OF TURBINE ZONE AND
COMPRESSOR ZONE OF TURBO-COMPRESSOR WITH GENERAL IMPELLER FOR GAS TURBINE ENGINES |
ÐÅÇÓËÜÒÀÒÈ
ÄÎÑË²ÄÆÅÍÜ ÒÓÐÁ²ÍÍί ÒÀ ÊÎÌÏÐÅÑÎÐÍί ×ÀÑÒÈÍ ÒÓÐÁÎÊÎÌÏÐÅÑÎÐÀ ²Ç ÑϲËÜÍÈÌ
ÐÎÁÎ×ÈÌ ÊÎËÅÑÎÌ ÄËß ÇÀÑÒÎÑÓÂÀÍÍß Ó ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓÍÀÕ |
63–67 |
|
Êóëèêîâ Ã. Ã., |
ÌÅÒÎÄÈÊÀ ÏÎÁÓÄÎÂÈ ÍÅÉÐÎÌÅÐÅÆÅÂί ÌÎÄÅ˲
ÄÂÎÕÂÀËÜÍÎÃÎ ÃÒÄ ²Ç ÂÈÊÎÍÀÍÍßÌ ÓÌΠÑÒÐÓÊÒÓÐÍί ÀÄÅÊÂÀÒÍÎÑÒ² |
68–73 |
||
Òàðàñåíêî Ì. À., |
COMPARATIVE ANALYSIS OF PARTIAL MODES
FOR SINGLE-SHAFT AND MULTI-SHAFT TURBINE ENGINE WITH CHANGING
AMBIENT TEMPERATURE |
ÏÎвÂÍßËÜÍÈÉ ÀÍÀË²Ç ×ÀÑÒÊÎÂÈÕ ÐÅÆÈ̲Â
ÎÄÍÎÂÀËÜÍÎÃÎ ÒÀ ÌÍÎÃÎÂÀËÜÍÈÕ ÃÒÄ ÏÐÈ Ç̲Ͳ ÒÅÌÏÅÐÀÒÓÐÈ ÍÀÂÊÎËÈØÍÜÎÃÎ ÏβÒÐß |
74–79 |
|
Ìèðãîðîä Â. Ô., |
CALCULABLE
REALIZATION OF MATHEMATICAL MODELS OF STATE SPACE IN FORM HAMMERSHTEIN |
ÎÁ×ÈÑËÞÂÀËÜÍÀ
ÐÅÀ˲ÇÀÖ²ß ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÏÐÎÑÒÎÐÓ ÑÒÀÍ²Â Ó ÔÎÐ̲ ÃÀÌÌÅÐØÒÅÉÍÀ |
ÂÛ×ÈÑËÈÒÅËÜÍÀß
ÐÅÀËÈÇÀÖÈß ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÏÐÎÑÒÐÀÍÑÒÂÀ ÑÎÑÒÎßÍÈÉ Â ÔÎÐÌÅ ÃÀÌÌÅÐØÒÅÉÍÀ |
80–85 |
Ïàí³í Â. Â., |
FORMING OF NEURON-NETWORK MODEL OF HYDRAULIC-MECHANICAL AUTOMATIC
CONTROL AVIATION ENGINES SYSTEM |
ÔÎÐÌÈÐÎÂÀÍÈÅ ÍÅÉÐÎÑÅÒÅÂÎÉ ÌÎÄÅËÈ
ÃÈÄÐÎÌÅÕÀÍÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ ÀÂÒÎÌÀÒÈ×ÅÑÊÎÃÎ ÓÏÐÀÂËÅÍÈß ÀÂÈÀÖÈÎÍÍÛÌÈ ÄÂÈÃÀÒÅËßÌÈ |
86–90 |
|
Êîíîíûõèí Å. À. |
OPTIMIZATION OF
TURBOSHAFT CONTROL ALGORITHMS FOR ACCELERATIONS |
ÎÏÒÈ̲ÇÀÖ²ß ÏÐÎÃÐÀÌÈ ÊÅÐÓÂÀÍÍß ÒÂÀÄ ÍÀ
ÅÒÀϲ ÏÐȪÌÈÑÒÎÑÒ² |
91–94 |
|
Êîðîáêî Â. Â., |
CONTROL THERMOACOUSTIC THERMAL MACHINE
TYPE "ENGINE
- HEAT PUMPS" BASED ON FUZZY LOGIC |
ÑÈÑÒÅÌÀ ÓÏÐÀÂËÅÍÈß ÒÅÐÌÎÀÊÓÑÒÈ×ÅÑÊÎÉ
ÒÅÏËÎÂÎÉ ÌÀØÈÍÎÉ ÒÈÏÀ
«ÄÂÈÃÀÒÅËÜ - ÒÅÏËÎÂÎÉ ÍÀÑÎÑ» ÍÀ ÁÀÇÅ ÍÅ×ÅÒÊÎÉ ËÎÃÈÊÈ |
95–102 |
|
Íàçèí Â. È. |
ABOUT APPLICABILITY OF METHOD
N'YUTONA-RAFSONA FOR DETERMINATION OF PRESSURES IN CHAMBERS OF HYDROSTATODYNAMIC BEARING OF THE DOUBLED TYPE |
ÏÐÎ ÇÀÑÒÎÑÎÂͲÑÒÜ ÌÅÒÎÄÓ
ÍÜÞÒÎÍÀ-ÐÀÔÑÎÍÀ ÄËß ÂÈÇÍÀ×ÅÍÍß ÒÈÑÊÓ Â ÊÀÌÅÐÀÕ Ã²ÄÐÎÑÒÀÒÎIJÍÀ̲×ÍÎÃÎ
Ï²ÄØÈÏÍÈÊÀ ÇÄÂΪÍÎÃÎ ÒÈÏÓ |
103–107 |
|
Õàóñòîâà À. Í. |
CALIBRATION OF
FIBER-OPTIC SPECTROMETER FOR OPTICAL EMISSION SPECTROSCOPY METHOD OF ELECTRIC
PROPULSION |
ÊÀ˲ÁÐÓÂÀÍÍß ÂÎËÎÊÎÍÍÎ-ÎÏÒÈ×ÍÎÃÎ
ÑÏÅÊÒÐÎÌÅÒÐÀ ÄËß ÏÐÎÂÅÄÅÍÍß ÎÏÒÈ×Íί Å̲ѲÉÍί ÑÏÅÊÒÐÎÑÊÎϲ¯ ÅËÅÊÒÐÎÐÀÊÅÒÍÈÕ
ÄÂÈÃÓͲ |
108–112 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Åïèôàíîâ Ñ. Â., |
TURBOFAN
TECHNICAL CONDITION CONTROL BY ON-GROUND AUTOMATIC PARAMETRIC DIAGNOSIS
COMPLEX |
ÊÎÍÒÐÎËÜ ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ
ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀÇÅÌÍÈÌ ÀÂÒÎÌÀÒÈÇÎÂÀÍÈÌ ÊÎÌÏËÅÊÑÎÌ
ÏÀÐÀÌÅÒÐÈ×Íί IJÀÃÍÎÑÒÈÊÈ |
113–120 |
|
Ñòðåëåö Â. Å., |
TURBINE ENGINE
TECHNICAL STATE DIAGNOSIS PROBLEMS SOLVING METHODOLOGY UNDER UNCERTAINTY
INPUTS |
ÌÅÒÎÄÎËÎòß
ÐÎÇÂ’ßÇÀÍÍß ÇÀÄÀ× Ä²ÀÃÍÎÑÒÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ Â
ÓÌÎÂÀÕ ÍÅÂÈÇÍÀ×ÅÍÎÑÒ² ÂÕ²ÄÍÈÕ ÄÀÍÈÕ |
121–127 |
|
Àáäóëëàåâ Ï. Ø., |
APPLICATION OF
THE DEMPSTER-SHAFER THEORY ON FUSION OF THE AVIATION GAS TURBINE ENGINES’
HEALTH INFORMATION |
ÎÑÎÁËÈÂÎÑÒ² ÇÀÑÒÎÑÓÂÀÍÍß ÒÅÎв¯
ÄÅÌÏÑÒÅÐÀ-ØÅÔÅÐÀ ÄËß ÑÈÍÒÅÇÓ ²ÍÔÎÐÌÀÖ²¯ ÏÐÎ ÒÅÕͲ×ÍÈÉ ÑÒÀÍ ÃÒÄ |
ÎÑÎÁÅÍÍÎÑÒÈ
ÏÐÈÌÅÍÅÍÈß ÒÅÎÐÈÈ ÄÅÌÏÑÒÅÐÀ-ØÅÔÅÐÀ ÏÐÈ ÑÈÍÒÅÇÅ ÈÍÔÎÐÌÀÖÈÈ Î ÒÅÕÍÈ×ÅÑÊÎÌ
ÑÎÑÒÎßÍÈÈ ÃÒÄ |
128–132 |
Ãîëüöîâ À. Ñ., |
DIAGNOSTICS OF
TECHNICAL CONDITION OF THE MAIN SPOOL AND SERVOMOTOR OPENING OF WICKED GATE
HYDROUNIT |
IJÀÃÍÎÑÒÓÂÀÍÍß ÒÅÕͲ×ÍÎÃÎ ÑÒÀÍÓ
ÃÎËÎÂÍÎÃÎ ÇÎËÎÒÍÈÊÀ ² ÑÅÐÂÎÌÎÒÎÐÀ ÑÈÑÒÅÌÈ ÓÏÐÀÂ˲ÍÍß Â²ÄÊÐÈÒÒßÌ ÍÀÏÐÀÂËßÞ×ÎÃÎ
ÀÏÀÐÀÒÓ Ã²ÄÐÎÒÓÐÁ²ÍÈ |
133–138 |
|
Ïàï÷¸íêîâ À. Â., |
ADEQUACY ANALYSIS OF TRADITIONAL METHODS LIFETIME
DIAGNOSTIC OF GAS TURBINE ENGINE PARTS |
ÀÍÀË²Ç ÀÄÅÊÂÀÒÍÎÑÒ² ÒÐÀÄÈÖ²ÉÍÈÕ ÌÅÒÎIJÂ
IJÀÃÍÎÑÒÓÂÀÍÍß ÐÅÑÓÐÑÓ ÄÅÒÀËÅÉ ÃÒÄ |
ÀÍÀËÈÇ
ÀÄÅÊÂÀÒÍÎÑÒÈ ÒÐÀÄÈÖÈÎÍÍÛÕ ÌÅÒÎÄÎÂ ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈß ÐÅÑÓÐÑÀ ÄÅÒÀËÅÉ ÃÒÄ |
139–142 |
Ìóõòàðîâ Ï. Ø. |
BASIC DOMINANTS
IN MAKING DECISION BY AIR TRAFFIC CONTROLLER DURING ESTIMATING OF
UTILITY-SAFETY OF NORM OF ECHELONING OF AIR SPACE |
ÎÑÍÎÂͲ
ÄÎ̲ÍÀÍÒÈ Â ÏÐÈÉÍßÒÒ² вØÅÍÜ À²ÀÄÈÑÏÅÒ×ÅÐÎÌ ÏÐÈ ÎÖ²ÍÖ² ÊÎÐÈÑÍÎÑÒ²-ÁÅÇÏÅÊÈ
ÍÎÐÌÈ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÏÐÎÑÒÎÐÓ |
143–150 |
|
Ðåâà Î. Ì., |
FINDING OF BOARDER RISK LEVELS DURING
AIR SPACE FLIGHT LEVELS NORMS VIOLATION |
ÂÈÇÍÀ×ÅÍÍß
ÃÐÀÍÈ×ÍÈÕ Ð²ÂͲ ÐÈÇÈÊÓ Ï²Ä ×ÀÑ ÏÎÐÓØÅÍÍß ÍÎÐÌÈ ÅØÅËÎÍÓÂÀÍÍß ÏβÒÐßÍÎÃÎ
ÏÐÎÑÒÎÐÓ |
ÎÏÐÅÄÅËÅÍÈÅ ÃÐÀÍÈ×ÍÛÕ ÓÐÎÂÍÅÉ ÐÈÑÊÀ ÂÎ
ÂÐÅÌß ÍÀÐÖÓØÅÍÈß ÍÎÐÌÛ ÝØÅËÎÍÈÐÎÂÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ |
151–156 |
Óñòèìåíêî È. Ì. |
INFORMATION
CYBERNETIC MODEL OF ORGANIZATIONAL AIR NAVIGATION STRUCTURES |
²ÍÔÎÐÌÀÖ²ÉÍÎ-ʲÁÅÐÍEÒÈ×ÍÀ ÌÎÄÅËÜ ÎÐÃÀͲÇÀÖ²ÉÍÈÕ
ÀÅÐÎÍÀ²ÃÀÖ²ÉÍÈÕ ÑÒÐÓÊÒÓÐ |
ÈÍÔÎÐÌÀÖÈÎÍÍÎ-ÊÈÁÅÐÍÅÒÈ×ÅÑÊÀß
ÌÎÄÅËÜ ÎÐÃÀÍÈÇÀÖÈÎÍÍÛÕ ÀÝÐÎÍÀÂÈÃÀÖÈÎÍÍÛÕ ÑÒÐÓÊÒÓÐ |
157–167 |
Ãðóçäî È. Â., |
APPLICATION
PARALLEL COMPUTING TO THE PROBLEM OF AUTHORSHIP ESTABLISHMENT OF TEXTS |
ÇÀÑÒÎÑÓÂÀÍÍß ÏÀÐÀËÅËÜÍÈÕ ÎÁ×ÈÑËÅÍÜ ÄÎ
ÂÈвØÅÍÍß ÇÀÂÄÀÍÍß ÂÑÒÀÍÎÂËÅÍÍß ÀÂÒÎÐÑÒÂÀ ÒÅÊÑҲ |
ÏÐÈÌÅÍÅÍÈÅ
ÏÀÐÀËËÅËÜÍÛÕ ÂÛ×ÈÑËÅÍÈÉ Ê ÐÅØÅÍÈÞ ÇÀÄÀ×È ÓÑÒÀÍÎÂËÅÍÈß ÀÂÒÎÐÑÒÂÀ ÒÅÊÑÒΠ|
168–176 |
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè |
||||
Äìèòð³ºâ Ñ. Î., |
THE
PROCEDURES FORMALIZE AND IDENTIFY THE OPTIMAL
MAINTENANCE PROGRAM AIRCRAFT AND AIRCRAFT ENGINES |
ÔÎÐÌÀËÈÇÀÖÈß
ÏÐÎÖÅÄÓÐ È ÎÏÐÅÄÅËÅÍÈÅ ÎÏÒÈÌÀËÜÍÛÕ ÏÐÎÃÐÀÌÌ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß
ÂÎÇÄÓØÍÛÕ ÑÓÄÎÂ È ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
177–181 |
|
ßêóøåíêî Î. C., |
USING OF
IMPROVED MAINTANANCE QUALITY RATE FOR CHOOSING THE MOST OPTIMAL MANTANANCE
COMPANIES |
ÈÑÏÎËÜÇÎÂÀÍÈÅ ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÍÎÃÎ
ÏÎÊÀÇÀÒÅËß ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÄËß ÎÁÎÑÍÎÂÀÍÎÃÎ ÂÛÁÎÐÀ ÎÏÒÈÌÀËÜÍÛÕ
ÐÅÌÎÍÒÍÛÕ ÏÐÅÄÏÐÈßÒÈÉ |
182–186 |
|
187 |
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
áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé
áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ
Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.