Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ
ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 9 (126). – 171 ñ.
ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È
ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 9 (126). – 171 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND
TECHNOLOGY. – 2015. – ¹ 9 (126). – 171 ñ.
Ìàòåðèàëû, ñîäåðæàùèåñÿ
â æóðíàëå, îïóáëèêîâàíû
ïî ðåøåíèþ XX ìåæäóíàðîäíîãî êîíãðåññà äâèãàòåëåñòðîèòåëåé
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè (article
title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà ìîâà |
Ðóññêèé
ÿçûê |
||
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Êîáçàðü Þ. Ì. |
TO ASSESS THE DURABILITY TO FATIGUE SMOOTH
CYLINDRICAL RODS UNDER UNIAXIAL SYMMETRIC STRETCH – COMPRESSION |
ÄÎ
ÎÖ²ÍÊÈ ÄÎÂÃβ×ÍÎÑÒ² ÏÐÈ ÂÒÎ̲ ÃËÀÄÊÈÕ ÖÈ˲ÍÄÐÈ×ÍÈÕ ÑÒÅÐÆÍ²Â ÏÐÈ ÎÄÍβÑÍÎÌÓ
ÑÈÌÅÒÐÈ×ÍÎÌÓ ÐÎÇÒßÃÓ-ÑÒÈÑÊÓ |
6–14 |
|
Ïîâãîðîäíèé Â. Î. |
MODERN AREAS OF
APPENDIX OF REVERSE TASKS OF MECHANICS AND THERMOMECHANICS |
ÑÓ×ÀÑͲ ÃÀËÓDz ÂÈÊÎÐÈÑÒÀÍÍß ÎÁÅÐÍÅÍÈÕ ÇÀÄÀ×
ÌÅÕÀͲÊÈ ÒÀ ÒÅÐÌÎÌÅÕÀͲÊÈ |
ÑÎÂÐÅÌÅÍÍÛÅ ÎÁËÀÑÒÈ ÏÐÈËÎÆÅÍÈß ÎÁÐÀÒÍÛÕ ÇÀÄÀ× ÌÅÕÀÍÈÊÈ È ÒÅÐÌÎÌÅÕÀÍÈÊÈ |
15–19 |
Ïîïóãà À. È. |
MAIN
DIRECTIONS OF REDUCTION OF AIRCRAFT NOISE |
ÎÑÍÎÂͲ ÍÀÏÐßÌÊÈ ÇÌÅÍØÅÍÍß
ØÓÌÓ ÏβÒÐßÍÈÕ ÑÓÄÅÍ |
20–25 |
|
Õîðÿê
Í. Â., |
THEORETICAL
EFFICIENCY ESTIMATION OF DYNAMIC DAMPER OF POGO
VIBRATIONS OF LIQUID ROCKET LAUNCH VECHICLE |
ÒÅÎÐÅÒÈ×ÍÀ ÎÖ²ÍÊÀ ÅÔÅÊÒÈÂÍÎÑÒ²
ÄÈÍÀ̲×ÍÎÃÎ ÃÀÑÈÒÅËß ÏÎÇÄÎÂÆÍ²Õ ÊÎËÈÂÀÍÜ Ð²ÄÈÍÍÈÕ ÐÀÊÅÒ-ÍÎѲ¯Â |
26–32 |
|
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ãàéäóê Ñ. Â., |
APPLICATION OF ANALITIC METHODS TO CALCULATE OF
CHEMICAL COMPOSITION γ-, γ'- PHASES AND PARAMETRIES PHASE STABILITIES CASTING NI-BASED SUPERALLOYS |
ÇÀÑÒÎÑÓÂÀÍÍß ÀÍÀ˲ÒÈ×ÍÈÕ ÌÅÒÎIJ ÄËß
ÐÎÇÐÀÕÓÍÊÓ Õ²Ì²×ÍÎÃÎ ÑÊËÀÄÓ γ-, γ'- ÔÀÇ ÒÀ ÏÀÐÀÌÅÒв ÔÀÇÎÂί
ÑÒÀÁ²ËÜÍÎÑÒ² ËÈÂÀÐÍÈÕ ÆÀÐÎ̲ÖÍÈÕ Í²ÊÅËÅÂÈÕ ÑÏËÀ² |
33–37 |
|
Ôðîëîâ
Ã. À., |
IDENTIFICATION OF THERMOPHYSICAL
PROPERTIES OF HONEYCOMB STRUCTURE SAMPLES WITHIN TEMPERATURE RANGING BETWEEN
-60 AND + 250 °C AND UNDER PRESSURE BETWEEN 105
TO 10-1 PA |
ÂÈÇÍÀ×ÅÍÍß ÒÅÏËÎÔ²ÇÈ×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÇÐÀÇʲ ÑÒ²ËÜÍÈÊÎÂÈÕ ÊÎÍÑÒÐÓÊÖ²É Â Ä²ÀÏÀÇÎͲ ÒÅÌÏÅÐÀÒÓÐ -60 ... + 250 ° Ñ ²
ÒÈÑÊÓ Â²Ä 105 ÄÎ 10-1 ÏÀ |
38–43 |
|
Ñîðîêèí
Â. Ô., |
CREATING SMOOTH LAW
CHANGES JERK IN THE INTERVAL OF ACCELERATION/DECELERATION IN HIGH-SPEED MACHINING ON CNC EQUIPMENT |
ÔÎÐÌÓÂÀÍÍß ÃËÀÄÊÎÃÎ ÇÀÊÎÍÓ
Ç̲ÍÈ ÐÈÂÊÀ ÍÀ IJËÜÍÈÖßÕ ÐÎÇÃÎÍÓ- ÃÀËÜÌÓÂÀÍÍß ÏÐÈ
ÂÈÑÎÊÎØÂÈÄʲÑÍ²É ÎÁÐÎÁÖ² ÍÀ ÎÁËÀÄÍÀÍͲ Ç ×ÏÓ |
44–50 |
|
Ïëàíêîâñêèé
Ñ. È., |
MATHEMATICAL MODEL OF EDGE FINISHING WITH THERMAL-PULSE TREATMENT |
ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÎÏÎÐßÄÆÅÍÍß ÊÐÀÉÎÊ
ÏÐÈ ÒÅÐÌβÌÏÓËÜÑÍ²É ÎÁÐÎÁÖ² |
ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÎÒÄÅËÊÈ
ÊÐÎÌÎÊ ÏÐÈ ÒÅÐÌÎÈÌÏÓËÜÑÍÎÉ ÎÁÐÀÁÎÒÊÅ |
51–55 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Òåðåøèí À. Ì. |
ESTIMATION
OF MAIN VEHICLE PERFORMANCE CHARACTERISTICS (THRUST, LIFT-TO-DRAG RATIO,
RANGE) BY USING RESULTS OF RAMJET BRANCH TESTING |
ÎÖ²ÍÊÀ ÎÑÍÎÂÍÈÕ ËÜÎÒÍÎ-ÒÅÕͲ×ÍÈÕ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ (ÒßÃÀ, ßʲÑÒÜ, ÄÀËÜͲÑÒÜ) ˲ÒÀËÜÍÎÃÎ ÀÏÀÐÀÒÓ ÇÀ ÐÅÇÓËÜÒÀÒÀÌÈ
ÂÎÃÍÅÂÈÕ ÑÒÅÍÄÎÂÈÕ ÂÈÏÐÎÁÓÂÀÍÜ ÏÐßÌÎÒÎ×ÍÈÕ ÏβÒÐßÍÎ-ÐÅÀÊÒÈÂÍÈÕ ÄÂÈÃÓͲ |
56–59 |
|
Êóëèê À. Ñ., |
FRACTIONAL
ORDER TRANSFER FUNCTION USAGE FOR SYNTHESIS OF THE AUTOMATIC POSITIONING
SYSTEM OF OPERATING MODE OF VORTICAL POWER
SEPARATOR |
ÂÈÊÎÐÈÑÒÀÍÍß ÏÅÐÅÄÀÒÎ×ÍÈÕ ÔÓÍÊÖ²É
ÄÐÎÁÎÂÎÃÎ ÏÎÐßÄÊÓ ÄËß ÂÈвØÅÍÍß ÇÀÄÀײ ÑÈÍÒÅÇÓ ÑÈÑÒÅÌÈ ÏÎÇÈÖ²ÞÂÀÍÍß
ÐÅÆÈ̲ ÂÈÕÐÎÂÎÃÎ ÅÍÅÐÃÎÐÎÇIJËÞÂÀ×À |
60–66 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Æàðèêîâ Â. Í. |
AERODERIVATIVE GAS TURBINES. SCOPE OF APPLICATION. STANDARDS |
À²ÀÖ²ÉͲ ÊÎÍÂÅÐÒÎÂÀͲ ÃÀÇβ ÒÓÐÁ²ÍÈ.
ÑÔÅÐÀ ÇÀÑÒÎÑÓÂÀÍÍß. ÑÒÀÍÄÀÐÒÈ |
ÀÂÈÀÖÈÎÍÍÛÅ ÊÎÍÂÅÐÒÈÐÎÂÀÍÍÛÅ ÃÀÇÎÂÛÅ ÒÓÐÁÈÍÛ. ÑÔÅÐÀ ÏÐÈÌÅÍÅÍÈß. ÑÒÀÍÄÀÐÒÛ |
67–74 |
Ðóñàíîâ À. Â., |
RESEARCH OF STREAM FLOW STRUCTURE IN REGULATIVE COMPARTMENT OF THE HPC OF STEAM TURBINE Ê-325-23,5 WITH PARTIAL 0,4 |
ÄÎÑË²ÄÆÅÍÍß
ÑÒÐÓÊÒÓÐÈ ÏÎÒÎÊÓ Â ÐÅÃÓËÞÞ×ÎÌÓ Â²ÄѲÊÓ ÖÂÒ ÏÀÐÎÂί
ÒÓÐÁ²ÍÈ Ê-325-23,5 ÍÀ ÐÅÆÈ̲ ÏÀÐÖ²ÀËÜÍÎÑÒ² 0,4 |
75–80 |
|
Ñàâ÷åíêî Ê. Â., |
INFLUENCE OF THE
TYPE OF
SHROUDS ON THE STATIC STRESS STATE OF BLADE RINGS |
ÂÏËÈÂ ÒÈÏÓ ÁÀÍÄÀÆÍÈÕ ÏÎËÈÖÜ ÍÀ
ÑÒÀÒÈ×ÍÈÉ ÍÀÏÐÓÆÅÍÈÉ ÑÒÀÍ ËÎÏÀÒÊÎÂÈÕ Â²Íֲ |
ÂËÈßÍÈÅ ÒÈÏÀ ÁÀÍÄÀÆÍÛÕ ÏÎËÎÊ ÍÀ
ÑÒÀÒÈ×ÅÑÊÎÅ ÍÀÏÐ߯ÅÍÍÎÅ ÑÎÑÒÎßÍÈÅ ËÎÏÀÒÎ×ÍÛÕ ÂÅÍÖΠ|
81–84 |
Íàçèí Â. È. |
COMPARISON OF DYNAMIC DESCRIPTIONS OF THE DOUBLED
AND SINGLE HYDROSTATODINAMIC BEARINGS |
ÏÎвÂÍßÍÍß ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÇÄÂΪÍÈÕ
² ÎÄÈÍÀÐÍÈÕ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÈÕ Ï²ÄØÈÏÍÈʲ |
ÑÐÀÂÍÅÍÈÅ
ÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÄÂÎÅÍÍÛÕ
È ÎÄÈÍÀÐÍÛÕ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÈÕ
ÏÎÄØÈÏÍÈÊÎÂ |
85–88 |
Ñèðåíêî
Ô. Ô., |
SYNTHESIS TECHNIC
OF A TORQUE MEASURING ALGORITHM FOR A TORQUE MEASURING UNIT, WHICH IMPLEMENTS THE PHASE METERING
PRINCIPLE, IN CONDITIONS OF LIMITED INFORMATION ABOUT THE PROPERTIES
OF UNIT |
ÑÈÍÒÅÇ ÀËÃÎÐÈÒÌÓ ÂÈÇÍÀ×ÅÍÍß ÂÅËÈ×ÈÍÈ ÊÐÓÒÈËÜÍÎÃÎ ÌÎÌÅÍÒÓ ÔÀÇÎÌÅÒÐÈ×ÍÈÌ
ÌÅÒÎÄÎÌ Â ÓÌÎÂÀÕ ÎÁÌÅÆÅÍί ²ÍÔÎÐÌÀÖ²¯ ÏÐÎ ÂËÀÑÒÈÂÎÑÒ² ÂÈ̲ÐÞÂÀ×À |
89–97 |
|
Sumtsov A., |
MODEL BASED DESIGN APPROACH APPLIED ON THE DEVELOPMENT
OF THE ENGINE MONITORING MODULE |
ÇÀÑÒÎÑÓÂÀÍÍß ÌÎÄÅËÜÍÎ-ÎвªÍÒÎÂÀÍÎÃÎ
ÏÐÎÅÊÒÓÂÀÍÍß ÄËß ÐÎÇÐÎÁÊÈ ÁËÎÊÀ ÊÅÐÓÂÀÍÍß ÄÂÈÃÓÍÀ ˲ÒÀÊÀ |
ÏÐÈÌÅÍÅÍÈÅ ÌÎÄÅËÜÍÎ-ÎÐÈÅÍÒÈÐÎÂÀÍÍÎÃÎ
ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÄËß ÐÀÇÐÀÁÎÒÊÈ
ÁËÎÊÀ ÓÏÐÀÂËÅÍÈß ÑÀÌÎ˨ÒÍÎÃÎ
ÄÂÈÃÀÒÅËß |
98–102 |
Ëîÿí À. Â. |
POSSIBILITY INVESTIGATION
OF HALL EFFECT THRUSTER DIRECT ELECTRIC POWER SUPPLYING (WITHOUT INTERMEDIATE CONVERTERS) FROM SOLAR BATTERY |
ÄÎÑË²ÄÆÅÍÍß ÌÎÆËÈÂÎÑÒ² ÁÅÇÏÎÑÅÐÅÄÍÜÎÃÎ
ÅËÅÊÒÐÎÆÈÂËÅÍÍß (ÁÅÇ ÏÐÎ̲ÆÍÈÕ ÏÅÐÅÒÂÎÐÞÂÀײÂ) ÄÂÈÃÓÍÀ ÕÎË˲ÂÑÜÊÎÃÎ
ÒÈÏÓ Â²Ä ÂÈÑÎÊÎÂÎËÜÒÍί ÁÀÒÀÐů ÔÎÒÎÅËÅÊÒÐÈ×Íί |
103–107 |
|
Íåðóáàññêèé Â. Â. |
USING
MAHALANOBIS-TAGUCHI SYSTEM IN
TASKS RELATED TO THE TURBINE
ENGINE FAULT RECOGNITION |
ÂÈÊÎÐÈÑÒÀÍÍß ÑÈÑÒÅÌÈ ÌÀÕÀËÀÍÎÁ²ÑÀ-ÒÀÃÓÒ² Ó ÇÀÄÀ×ÀÕ ÐÎÇϲÇÍÀÂÀÍÍß ÍÅÑÏÐÀÂÍÎÑÒÅÉ
ÃÒÄ |
ÈÑÏÎËÜÇÎÂÀÍÈÅ ÑÈÑÒÅÌÛ ÌÀÕÀËÀÍÎÁÈÑÀ-ÒÀÃÓÒÈ Â ÇÀÄÀ×ÀÕ ÐÀÑÏÎÇÍÀÂÀÍÈß
ÍÅÈÑÏÐÀÂÍÎÑÒÅÉ ÃÒÄ |
108–112 |
Õàóñòîâà À. Í. |
DEVELOPMENT OF
HIGH RESOLUTION SPECTRAL COMPLEX FOR THE STATIONARY PLASMA THRUSTER SPECTRUM
RESEARCH |
ÐÎÇÐÎÁÊÀ
ÑÏÅÊÒÐÀËÜÍÎÃÎ ÊÎÌÏËÅÊÑÓ ÂÈÑÎÊÎÃÎ ÐÎÇIJËÅÍÍß ÄËß ÄÎÑË²ÄÆÅÍÍß ÑÏÅÊÒÐÓ
ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ |
113–118 |
|
ßêóøåíêî
Î. Ñ., |
THE MODELLING
OF ACCUMULATION OF AVIATION ENGINE’S DAMAGES AT
DIFFERENT LAWS OF CONTROL BY ITS OPERATION DURING TAKE-OFF |
ÌÎÄÅËÞÂÀÍÍß
ÏÐÎÖÅѲ ÍÀÊÎÏÈ×ÅÍÍß ÏÎØÊÎÄÆÅÍÜ ÍÀ ÇËÜÎÒ² ÏÐÈ ÂÈÊÎÐÈÑÒÀÍͲ вÇÍÈÕ ÇÀÊÎͲÂ
ÓÏÐÀÂ˲ÍÍß ÃÒÄ |
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÏÐÎÖÅÑÑΠÍÀÊÎÏËÅÍÈß ÏÎÂÐÅÆÄÅÍÍÎÑÒÅÉ ÍÀ ÂÇËÅÒÅ ÏÐÈ ÈÑÏÎËÜÇÎÂÀÍÈÈ ÐÀÇËÈ×ÍÛÕ ÇÀÊÎÍΠÓÏÐÀÂËÅÍÈß ÃÒÄ |
119–122 |
Òêà÷ Ì. Ð., |
PERFORMANCE OF
THE WORKING FLUID FOR METAL HYDRIDE UTILIZATION CONTINUOUS PLANT |
ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÐÎÁÎ×ÎÃÎ Ò²ËÀ ÌÅÒÀËÎòÄÐÈÄÍί ÓÒÈ˲ÇÀÖ²ÉÍί ÓÑÒÀÍÎÂÊÈ ÁÅÇÏÅÐÅÐÂÍί IJ¯ |
ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÐÀÁÎ×ÅÃÎ ÒÅËÀ ÌÅÒÀËËÎÃÈÄÐÈÄÍÎÉ ÓÒÈËÈÇÀÖÈÎÍÍÎÉ
ÓÑÒÀÍÎÂÊÈ ÍÅÏÐÅÐÛÂÍÎÃÎ ÄÅÉÑÒÂÈß |
123–128 |
Áîðçîâ Ñ. À. |
SPECTRAL-CORRELATION
METHOD ESTIMATION OF EFFECTIVE WORK THE COMBUSTION CHAMBER OF GAS TURBINE
ENGINE |
ÑÏÅÊÒÐÀËÜÍÎ-ÊÎÐÅËßÖ²ÉÍÈÉ ÌÅÒÎÄ ÎÖ²ÍÊÈ
ÅÔÅÊÒÈÂÍÎÑÒ² ÐÎÁÎÒÈ ÂÓÇËÀ ÊÀÌÅÐÈ ÇÃÎÐßÍÍß ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ |
129–135 |
|
ªí÷åâ
Ñ. Â., |
PROGNOSTIC VIBRATION STATE OF KNOTS AVIATION
ENGINES GAS-TURBINES AFTER
PARAMETERS OF
WAVELET-DECOMPOSITION |
ÏÐÎÃÍÎÇÓÂÀÍÍß Â²ÁÐÎÑÒÀÍÓ ÂÓÇ˲ À²ÀÖ²ÉÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÇÀ
ÏÀÐÀÌÅÒÐÀÌÈ ÂÅÉÂËÅÒ-ÐÎÇÊËÀÄÓ |
ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÂÈÁÐÎÑÎÑÒÎßÍÈß ÓÇËÎÂ
ÀÂÈÀÖÈÎÍÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÏÎ ÏÀÐÀÌÅÒÐÀÌ ÂÅÉÂËÅÒ-ÐÀÇËÎÆÅÍÈß |
136–140 |
Òàðàñåíêî À. È., |
PARTIAL MODES
OF OPERATION OF THE COMPRESSORS
ON A SINGLE-SHAFT TURBINE
ENGINE OR TURBINE ENGINE WITH A FREE POWER
TURBINE WORKING WITH VARYING TEMPERATURES OF OUTSIDE AIR |
ÐÎÁÎÒÀ ÊÎÌÏÐÅÑÎÐÀ ÍÀ ×ÀÑÒÊÎÂÈÕ ÐÅÆÈÌÀÕ
ÎÄÍÎÂÀËÜÍÎÃÎ ÃÒÄ ÒÀ ÃÒÄ Ç
²ËÜÍÎÞ ÑÈËÎÂÎÞ ÒÓÐÁ²ÍÎÞ ÏÐÈ Ç̲Ͳ ÒÅÌÏÅÐÀÒÓÐÈ ÇÎÂͲØÍÜÎÃÎ ÏβÒÐß |
141–144 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Áàáåíêî Þ. Â. |
THE
METHOD OF VALUATION OF MODIFICATIONS SHORT-HAUL PASSENGER AIRCRAFT |
ÌÅÒÎÄÈÊÀ ÂÀÐÒ²ÑÍί
ÎÖ²ÍÊÈ ÌÎÄÈÔ²ÊÀÖ²É ÁËÈÇÜÊÎÌÀòÑÒÐÀËÜÍÈÕ ÏÀÑÀÆÈÐÑÜÊÈÕ
˲ÒÀʲ |
ÌÅÒÎÄÈÊÀ ÑÒÎÈÌÎÑÒÍÎÉ ÎÖÅÍÊÈ ÌÎÄÈÔÈÊÀÖÈÉ ÁËÈÆÍÅÌÀÃÈÑÒÐÀËÜÍÛÕ
ÏÀÑÑÀÆÈÐÑÊÈÕ ÑÀÌÎËÅÒÎÂ |
145–148 |
Ëîãèíîâ Â. Â. |
SOFTWARE
FOR FORMING OF OPERATIONAL PERFORMANCE
OF ENGINE
AIRCRAFT POWER PLANT |
ÏÐÎÃÐÀÌÍÈÉ ÊÎÌÏËÅÊÑ ÏÎ ÔÎÐÌÓÂÀÍÍÞ ÅÊÑÏËÓÀÒÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ
ÄÂÈÃÓÍÀ ÑÈËÎÂί ÓÑÒÀÍÎÂÊÈ
˲ÒÀÊÀ |
149–152 |
|
Ðåâà Î. Ì., |
PILOT ANALYSIS
OF AIR TRAFFIC CONTROLLERS DESIRABILITY LEVELS ON THE SPECTER
OF THE HORIZONTAL AIR SPACE FLIGHT SEPARATION NORMS |
ÏÈËÎÒÍÛÉ
ÀÍÀËÈÇ ÓÐÎÂÍÅÉ ÏÐÈÒßÇÀÍÈÉ ÀÂÈÀÄÈÑÏÅÒ×ÅÐΠÍÀ ÑÏÅÊÒÐÅ ÃÎÐÈÇÎÍÒÀËÜÍÈÕ
ÍÎÐÌ ÝØÅËÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ |
153–160 |
|
Òðåòüÿê
Â. Â., |
THE POSSIBILITY
OF INTERACTIVE SOFTWARE SYSTEMS FOR THE DESIGN PULSE PROCESSES TO MANUFACTURE
COMPLEX PARTS BY ADDRESSING AND SYNTHESIS |
ÌÎÆËÈÂÎÑÒ² ²ÍÒÅÐÀÊÒÈÂÍÎÃÎ ÏÐÎÃÐÀÌÍÎÃÎ
ÊÎÌÏËÅÊÑÓ ÄËß ÏÐÎÅÊÒÓÂÀÍÍß ÒÅÕÍÎËÎò×ÍÈÕ ÏÐÎÖÅѲ ²ÌÏÓËÜÑÍί ÎÁÐÎÁÊÈ ÏÐÈ
ÂÈÃÎÒÎÂËÅÍͲ ÑÊËÀÄÍÈÕ ÄÅÒÀËÅÉ ÌÅÒÎÄÎÌ ÀÄÐÅÑÀÖ²¯ ÒÀ ÑÈÍÒÅÇÓ |
161–165 |
|
Ôåäîðîâè÷ Î. Å., |
THE RATIONAL ALLOCATION OF FUNDS TO IMPROVE
THE QUALITY OF PRODUCTS TO
DEVELOP THE ENTERPRISE |
ÐÀÖ²ÎÍÀËÜÍÈÉ ÐÎÇÏÎÄ²Ë ÊÎØÒ²Â ÄËß
ÏÎÊÐÀÙÅÍÍß ßÊÎÑÒ² ÏÐÎÄÓÊÖ²¯ ϲÄÏÐȪÌÑÒÂÀ, ÙÎ ÐÎÇÂÈÂÀªÒÜÑß |
166–169 |
|
170 |
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 (ïðèêàç ÌÎÍ Óêðàèíû ¹1279 îò 6.11.2014 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 (ICV 2013: 4,83) (Ïîëüøà); Google Scholar (áèáëèîìåòðè÷åñêèå ïîêàçàòåëè – quot.=2094 / h
= 10 / i10 = 15).