Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2013. – ¹ 7(104). – 256 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 7(104). –
256 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 7(104). – 256 ñ.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ìàêàåâà Ð.Õ., |
application of holographic interferometry for the testing of quality
of the soldered and welded joint |
ÂÈÊÎÐÈÑÒÀÍÍß
ãîëîãðàô²÷Íî¯ ²íòåðôåðîìåò𲯠äëÿ êîíòðîëÞ ßêÎÑÒ² ïàÿíÈõ ² ÇÂÀÐÍÈÕ ç’ºäíàíü |
ÏÐÈÌÅÍÅÍÈÅ
ÃÎËÎÃÐÀÔÈ×ÅÑÊÎÉ ÈÍÒÅÐÔÅÐÎÌÅÒÐÈÈ ÄËß ÊÎÍÒÐÎËß ÊÀ×ÅÑÒÂÀ ÏÀßÍÛÕ È ÑÂÀÐÍÛÕ
ÑÎÅÄÈÍÅÍÈÉ |
7–11 |
Ãóñàðåâ Â.Ñ., |
Experimental study of dependence of technological
system action of form-building modes |
åêñïåð³ìåíòàëüíå
äîñë³äæåííÿ çàëåæíîñò³ 䳿 òåõíîëîã³÷íî¿ ñèñòåìè â³ä ðåæèì³â ôîðìîóòâîðåííÿ |
12–16 |
|
Êàëèíèíà Í.Å., |
MATERIAL
SCIENCE ASPECTS OF NANOMODIFICATION MULTICOMPONENT NICKEL ALLOYS |
ÌÀÒÅвÀËÎÇÍÀÂײ ÀÑÏÅÊÒÈ
ÍÀÍÎÌÎÄÈÔ²ÊÓÂÀÍÍß ÁÀÃÀÒÎÊÎÌÏÎÍÅÍÒÍÈÕ Í²ÊÅËÅÂÈÕ ÑÏËÀ² |
ÌÀÒÅÐÈÀËÎÂÅÄ×ÅÑÊÈÅ
ÀÑÏÅÊÒÛ ÍÀÍÎÌÎÄÈÔÈÖÈÐÎÂÀÍÈß ÌÍÎÃÎÊÎÌÏÎÍÅÍÒÍÛÕ ÍÈÊÅËÅÂÛÕ ÑÏËÀÂÎÂ |
17–21 |
Ìîçãîâîé Â.Ô., |
STRATEGY OF PROCESSING
OF BLADES MONOWHELS ON THE PROCESSING CENTRES CNC WITH VARIABLE 3D-CORRECTION |
ÑÒÐÀÒÅÃII ÎÁÐÎÁÊÈ ËÎÏÀÒÎÊ
ÌÎÍÎÊÎËÅÑ ÍÀ ÎÁÐÎÁËÞÂÀÍÍÈÕ ÖÅÍÒÐÀÕ Ç ×ÏÊ Ç ÌIÍËÈÂÎÞ 3D-ÊÎÐÅÊÒÓÐÎÞ |
ÑÒÐÀÒÅÃÈÈ ÎÁÐÀÁÎÒÊÈ
ËÎÏÀÒÎÊ ÌÎÍÎÊÎ謄 ÍÀ ÎÁÐÀÁÀÒÛÂÀÞÙÈÕ ÖÅÍÒÐÀÕ Ñ ×ÏÓ Ñ ÏÅÐÅÌÅÍÍÎÉ 3D-ÊÎÐÐÅÊÖÈÅÉ |
22–28 |
Íàáîêèíà Ò.Ï., |
SPEED OF THE UNHARDERING CUTTING BY SUPERSONIC HIGH-TEMPERATURE STREAMS
OF THE MATERIALS BASED ON ALUMINUM ALLOYS |
ØÂÈÄʲÑÒÜ Ð²ÇÊÈ ÇÍÅ̲ÖÍÞÂÀÍÍßÌ
ÍÀÄÇÂÓÊÎÂÈÌÈ ÂÈÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÈÌÈ ÃÀÇÎÂÈÌÈ ÑÒÐÓÌÈÍÀÌÈ ÌÀÒÅвÀ˲ ÍÀ ÎÑÍβ
ÀËÞ̲ͲªÂÈÕ ÑÏËÀ² |
29–32 |
|
Ñîðîêèí Â.Ô., |
SYNTHESIS OF
INVOLUTE PATHS OF HIGH-SPEED MACHINING OF HOLES |
ÑÈÍÒÅÇ ÅÂÎËÜÂÅÍÒÍÈÕ ÒÐÀªÊÒÎвÉ
ÂÈÑÎÊÎØÂÈÄʲÑÍÎÃÎ ÔÐÅÇÅÐÓÂÀÍÍß ÎÒÂÎв |
ÑÈÍÒÅÇ ÝÂÎËÜÂÅÍÒÍÛÕ
ÒÐÀÅÊÒÎÐÈÉ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÎÉ ÐÀÑÔÐÅÇÅÐÎÂÊÈ ÎÒÂÅÐÑÒÈÉ |
33–38 |
Áûáèí À.À., |
Optimization of the chemical etching process PROTECTIVE COATINGS FOR
generalized criteria |
ÎÏÒÈ̲ÇÀÖ²ß
ïðîöåñó õ³ì³÷íîãî òðàâëåííÿ ÇÀÕÈÑÍÎÃÎ ÏÎÊÐÈÒÒß ÇÀ óçàãàëüíåíÈÌ êðèòåð³ªÌ |
ÎÏÒÈÌÈÇÀÖÈß ÏÐÎÖÅÑÑÀ
ÕÈÌÈ×ÅÑÊÎÃÎ ÒÐÀÂËÅÍÈß ÇÀÙÈÒÍÎÃÎ ÏÎÊÐÛÒÈß ÏÎ ÎÁÎÁÙÅÍÍÎÌÓ ÊÐÈÒÅÐÈÞ |
39–42 |
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Ðîäèòåëåâ Â.È., |
CONSTRUCTIVE WAY TO LOWER LIFE CYCLE
COST OF MODERN AND ADVANCED AIR PROPULSION ENGINE |
ÊÎÍÑÒÐÓÊÒÈÂͲ ÑÏÎÑÎÁÈ ÇÍÈÆÅÍÍß ÂÀÐÒÎÑÒ²
ÆÈÒÒªÂÎÃÎ ÖÈÊËÓ ÑÓ×ÀÑÍÈÕ ² ÏÅÐÑÏÅÊÒÈÂÍÈÕ ÏÐÄ |
ÊÎÍÑÒÐÓÊÒÈÂÍÛÅ ÑÏÎÑÎÁÛ
ÑÍÈÆÅÍÈß ÑÒÎÈÌÎÑÒÈ ÆÈÇÍÅÍÍÎÃÎ ÖÈÊËÀ ÑÎÂÐÅÌÅÍÍÛÕ È ÏÅÐÑÏÅÊÒÈÂÍÛÕ ÂÐÄ |
43–52 |
Ñîðî÷êèí À.Í., |
ANALYSIS OF WAYS TO CARRY OUT MODERNIZATION OF
ATTACK AIRCRAFT SU- |
ÀÍÀË²Ç ØËßղ ÌÎÄÅÐͲÇÀÖ²¯ ˲ÒÀÊÀ ØÒÓÐÌÎÂÈÊÀ ÒÈÏÓ ÑÓ-25 Ç ÌÅÒÎÞ ÏÎÊÐÀÙÅÍÍß ÉÎÃÎ ÅÊÑÏËÓÀÒÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ |
53–60 |
|
Ãîðáåíêî À.Í. |
ON THE PERMISSIBLE LEVEL OF ANISOTROPY OF THE GYROSCOPIC INERTIA OF THE
ROTOR |
ÏÐÎ ÄÎÏÓÑÒÈÌÈÉ Ð²ÂÅÍÜ ²ÍÅÐÖ²ÉÍί
ÀͲÇÎÒÐÎϲ¯ òÐÎÑÊÎϲ×ÍÎÃÎ ÐÎÒÎÐÀ |
Î ÄÎÏÓÑÒÈÌÎÌ
ÓÐÎÂÍÅ ÈÍÅÐÖÈÎÍÍÎÉ ÀÍÈÇÎÒÐÎÏÈÈ ÃÈÐÎÑÊÎÏÈ×ÅÑÊÎÃÎ ÐÎÒÎÐÀ |
61–66 |
Ìîãèëüíèêîâ Â.Ï., |
AIR QUALITY FLIGHT RESEARCH METHODS, BLEED AIR FROM ENGINES FOR
AIRCRAFT AIR SYSTEM |
ÌÅÒÎÄÈÊÈ ËÜÎÒÍÈÕ ÂÈÏÐÎÁÓÂÀÍÜ ×ÈÑÒÎÒÈ
ÏβÒÐß, ßÊвÄÁÈÐÀªÒÜÑß Â²Ä À²ÀÖ²ÉÍÈÕ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲ ÍÀ ÏÎÒÐÅÁÈ ÑÈÑÒÅÌ
ÊÎÍÄÈÖ²ÞÂÀÍÍß ÏβÒÐßÍÈÕ ÑÓÄÅÍ |
67–72 |
|
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ãèðüêà Þ.Â., |
AERODYNAMIC
CHARACTERISTIC OF ENGINE BASED AT COANDA EFFECT |
ÀÅÐÎÄÈÍÀ̲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÄÂÈÃÓÍÀ
ÁÏËÀ, ÎÑÍÎÂÀÍÎÃÎ ÍÀ
ÅÔÅÊÒ² ÊÎÀÍÄÀ |
ÀÝÐÎÄÈÍÀÌÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ
ÄÂÈÃÀÒÅËß ÁÏËÀ, ÎÑÍÎÂÀÍÍÎÌ ÍÀ ÝÔÔÅÊÒÅ ÊÎÀÍÄÀ |
73–77 |
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Àë¸õèí Ñ.À., |
Auxiliary power units of vehicles and
prospects of their development |
ÄÎÏÎ̲ÆÍ² ñèëîâ³ óñòàíîâêè òðàíñïîðòíèõ çàñîá³â òà ïåðñïåêòèâè ¿õ
ðîçâèòêó |
ÂÑÏÎÌÎÃÀÒÅËÜÍÛÅ ÑÈËÎÂÛÅ
ÓÑÒÀÍÎÂÊÈ ÒÐÀÍÑÏÎÐÒÍÛÕ ÑÐÅÄÑÒÂ È ÏÅÐÑÏÅÊÒÈÂÛ ÈÕ ÐÀÇÂÈÒÈß |
78–82 |
Êèñëîâ Î.Â. |
THE GAS TURBINE
ENGINE GAS GENERATOR CHARACTERISTICS |
ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÃÒÄ |
83–86 |
|
Õàëàòîâ À.À., |
Adaptation of k-ε turbulence model for the flat plate film cooling
numerical simulations downstream two rows of holes arranged in spherical dimples |
ÀÄÀÏÒÀÖ²ß k-ε ÌÎÄÅ˲ ÒÓÐÁÓËÅÍÒÍÎÑÒ² ÄËß ÌÎÄÅËÞÂÀÍÍß ïë³âêîâîãî ÎÕÎËÎÄÆÅÍÍß
×ÅÐÅÇ ÑÈÑÒÅÌÓ Äâîðÿäíèõ ÎÒÂÎÐ²Â Ó ñôåðè÷íîìó ïîãëèáëåíèì |
87–91 |
|
Äîëìàòîâ Ä.À., |
INFLUENCE OF
THE HIGH-FREQUENCY DISCHARGE ON NOx GENERATION –
DISINTEGRATION MECHANISMS |
ÂÏËÈ ÂÈÑÎÊÎ×ÀÑÒÎÒÍÈÕ ÐÎÇÐßÄI ÍÀ
ÌÅÕÀͲÇÌÈ ÃÅÍÅÐÀÖ²¯ ÒÀ ÐÓÉÍÓÂÀÍÍß ÎÊÑÈIJ ÀÇÎÒÓ |
ÂËÈßÍÈÅ
ÂÛÑÎÊÎ×ÀÑÒÎÒÍÛÕ ÐÀÇÐßÄΠÍÀ ÌÅÕÀÍÈÇÌÛ ÃÅÍÅÐÀÖÈÈ È ÐÀÑÏÀÄÀ ÎÊÑÈÄΠÀÇÎÒÀ |
92–96 |
Êðàâ÷åíêî È.Ô., |
THE NUMERICAL AND
EXPEREMENTAL RESEARCH OF TURBINE EXHAUST DUCT OF TURBOFAN ENGINE |
ÐÎÇÐÀÕÓÍÊÎÂÎ-ÅÊÑÏÅÐèÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÇÀÒÓÐÁ²ÍÍÎÃÎ ÊÀÍÀËÓ ÒÐÄÄ |
ÐÀÑ×ÅÒÍÎ-ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ
ÈÑÑËÅÄÎÂÀÍÈÅ ÇÀÒÓÐÁÈÍÍÎÃÎ ÊÀÍÀËÀ ÒÐÄÄ |
97–102 |
Âàñèëüåâ È.Ï., |
method of fire certification test of aircraft engine pipes |
ìåòîäèêà
âîãíåâèõ ñåðòèô³êàö³éíèõ âèïðîáóâàíü òðóáîïðîâîä³â àâ³àö³éíîãî ÃÒÄ |
ÌÅÒÎÄÈÊÀ ÎÃÍÅÂÛÕ
ÑÅÐÒÈÔÈÊÀÖÈÎÍÍÛÕ ÈÑÏÛÒÀÍÈÉ ÒÐÓÁÎÏÐÎÂÎÄÎÂ ÀÂÈÀÖÈÎÍÍÎÃÎ ÃÒÄ |
103–106 |
Ãóñåâ Þ.À., |
RESISTIVE-STRAIN
SENSORS WITH BYPASSING-PROTECTION SCREEN |
ÒÅÍÇÎÐÅÇÈÑÒÎÐÈ Ç ÀÍÒ²ØÓÍÒÓÞ×ÈÌ ÅÊÐÀÍÎÌ |
107–111 |
|
Ëîÿí À.Â., |
ACCOUNTING METHOD FOR DETERMINATION OF EFFECTIVE THERMAL CONDUCTIVITY OF METAL-POROUS
EMITTERS IN CATHODES FOR ELCTRIC PROPULSION |
ÐÎÇÐÀÕÓÍÊÎÂÈÉ ÑÏÎѲÁ
ÂÈÇÍÀ×ÅÍÍß ÅÔÅÊÒÈÂÍί ÒÅÏËÎÏÐβÄÍÎÑÒ²
ÌÅÒÀËÎÏÎвÑÒÈÕ Å̲ÒÅв ÊÀÒÎIJÂ
ÅÐÄ |
ÐÀÑ×ÅÒÍÛÉ ÑÏÎÑÎÁ
ÎÏÐÅÄÅËÅÍÈß ÝÔÔÅÊÒÈÂÍÎÉ ÒÅÏËÎÏÐÎÂÎÄÍÎÑÒÈ ÌÅÒÀËËÎÏÎÐÈÑÒÛÕ ÝÌÈÒÒÅÐÎÂ ÊÀÒÎÄÎÂ
ÝÐÄ |
112–116 |
Íåñòåðåíêî Ñ.Þ., |
PARTICLES VELOCITY DISTRIBUTION FUNCTION MOMENTS EQUATIONS SET IN
RARIFIED MEDIUM OF INDUCTIVE SOURCES OF PLASMA, ELECTRONS AND IONS |
ÑÈÑÒÅÌÀ вÂÍßÍÜ ÔÓÍÊÖ²¯ ÐÎÇÏÎIJËÓ
×ÀÑÒÈÍÎÊ ÇÀ ØÂÈÄÊÎÑÒßÌÈ Ó ÐÎÇÐ²ÄÆÅÍÎÌÓ ÑÅÐÅÄÎÂÈÙ² ²ÍÄÓÊÖ²ÉÍÈÕ ÄÆÅÐÅË ÏËÀÇÌÈ,
ÅËÅÊÒÐÎͲ ÒÀ ²ÎͲ |
117–120 |
|
Ãîëîùàïîâ Â.Í., |
THE
DEVELOPMENT OF PEAK POWER ON BASE OF OPERATING UNITS OF TPS |
Ñòâîðåííÿ ï³êîâî¯ ïîòóæíîñò³ íà îñíîâ³
åíåðãîáëîê³â ÒÅÑ, ùî åêñïëóàòóþòüñÿ |
ÑÎÇÄÀÍÈÅ ÏÈÊÎÂÎÉ
ÌÎÙÍÎÑÒÈ ÍÀ ÎÑÍÎÂÅ ÝÊÑÏËÓÀÒÈÐÓÅÌÛÕ ÝÍÅÐÃÎÁËÎÊÎÂ ÒÝÑ |
121–126 |
Ðàä÷åíêî Ð.Í., |
EVALUATION OF COOLING POTENTIAL OF AIR
AT THE INLET OF LOW SPEED DIESEL ENGINE OF TRANSPORT SHIP |
ÎÖ²ÍÊÀ ÏÎÒÅÍÖÈÀËÓ ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß
ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ |
ÎÖÅÍÊÀ ÏÎÒÅÍÖÈÀËÀ
ÎÕËÀÆÄÅÍÈß ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß ÒÐÀÍÑÏÎÐÒÍÎÃÎ ÑÓÄÍÀ |
127–132 |
Ñèí÷åíêî Ñ.Â., |
CREATION OF MATHEMATICAL
MODELS OF DISCHARGE CHARACTERISTICS OF ELECTROCHEMICAL ACCUMULATORS OF
VARIOUS TYPES BY MEANS OF EQUIVALENT CIRCUITS |
ÏÎÁÓÄÎÂÀ ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÐÎÇÐßÄÍÈÕ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÅËÅÊÒÐÎղ̲×ÍÈÕ ÀÊÓÌÓËßÒÎв вÇÍÈÕ ÒÈϲ ÇÀ ÄÎÏÎÌÎÃÎÞ ÑÕÅÌ
ÇÀ̲ÙÅÍÍß |
133–138 |
|
Äçåíçåðñêèé Â.À., |
DEVELOPMENT OF NEW
TECHNOLOGIES IMPROVE THE MECHANICAL PROPERTIES OF BATTERY LEAD ALLOYS |
ÐÎÇÐÎÁÊÀ ÍÎÂÈÕ ÒÅÕÍÎËÎÃ²É Ï²ÄÂÈÙÅÍÍß
ÌÅÕÀͲ×ÍÈÕ ÂËÀÑÒÈÂÎÑÒÅÉ ÑÂÈÍÖÅÂÈÕ ÑÏËÀ² ÄËß ÀÊÓÌÓËßÒÎв |
ÐÀÇÐÀÁÎÒÊÀ ÍÎÂÛÕ
ÒÅÕÍÎËÎÃÈÉ ÏÎÂÛØÅÍÈß ÌÅÕÀÍÈ×ÅÑÊÈÕ ÑÂÎÉÑÒ ÑÂÈÍÖÎÂÛÕ ÑÏËÀÂΠÄËß ÀÊÊÓÌÓËßÒÎÐΠ|
139–143 |
Áèëîíåíêî Ð.À. |
THE USE OF
ALUMINUM IN CHEMICAL CURRENT SOURCE TO GENERATE HYDROGEN |
ÂÈÊÎÐÈÑÒÀÍÍß ÀËÞÌ²Í²Þ Â Õ²Ì²×ÍÎÌÓ
ÄÆÅÐÅ˲ ÑÒÐÓÌÓ ÄËß ÃÅÍÅÐÓÂÀÍÍß ÂÎÄÍÞ |
ÈÑÏÎËÜÇÎÂÀÍÈÅ
ÀËÞÌÈÍÈß Â ÕÈÌÈ×ÅÑÊÎÌ ÈÑÒÎ×ÍÈÊÅ ÒÎÊÀ ÄËß ÃÅÍÅÐÈÐÎÂÀÍÈß ÂÎÄÎÐÎÄÀ |
144–150 |
Ñûñîåâ Þ.À. |
CONDUCTING FILM GENERATION ON
THE NON-CONDUCTOR SURFACE OF STARTING INJECTOR OF
PLASMA SOURCES |
ÔÎÐÌÓÂÀÍÍß ÏÐβÄÍί Ï˲ÂÊÈ ÍÀ ÏÎÂÅÐÕͲ
IJÅËÅÊÒÐÈÊÀ ÏÓÑÊÎÂÎÃÎ ²ÍÆÅÊÒÎÐÀ ÄÆÅÐÅËÀ ÏËÀÇÌÈ |
ÔÎÐÌÈÐÎÂÀÍÈÅ ÏÐÎÂÎÄßÙÅÉ
ÏËÅÍÊÈ ÍÀ ÏÎÂÅÐÕÍÎÑÒÈ ÄÈÝËÅÊÒÐÈÊÀ ÏÓÑÊÎÂÎÃÎ ÈÍÆÅÊÒÎÐÀ ÈÑÒÎ×ÍÈÊÀ ÏËÀÇÌÛ |
151–156 |
Øåïåòîâ Þ.À., |
MODELLING OF INCOMING
ENERGY FROM THE SOLAR PANELS OF THE SMALL SPACECRAFT (MICROSATELLITE) FOR
EARTH REMOTE SENSING |
ÌÎÄÅËÞÂÀÍÍß ÅÍÅÐÃÎÏÐÈÕÎÄÓ Â²Ä ÑÎÍß×ÍÈÕ
ÁÀÒÀÐÅÉ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÓ ÊËÀÑÓ Ì²ÊÐÎÑÓÏÓÒÍÈÊ ÄËß ÄÈÑÒÀÍÖ²ÉÍÎÃÎ ÇÎÍÄÓÂÀÍÍß
ÇÅÌ˲ |
157–160 |
|
Ðÿáêîâ Â.È., |
ENERGETIC
CONDITIONS OF "COLD" FUSION |
ÒÀÕ²ÎÍÍÀ ÅÍÅÐÃ²ß – ÎÑÍÎÂÀ «ÕÎËÎÄÍÎÃλ
ÑÈÍÒÅÇÓ |
161–167 |
|
Äàíîâ À.Ñ. |
FUNDUMENTAL ENERGY LEVELS
OF MATTER |
ÔÓÍÄÀÌÅÍÒÀËÜͲ ÅÍÅÐÃÅÒÈ×Ͳ вÂͲ ÌÀÒÅв¯ |
168–171 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Ïîãîðåëîâ Ã.È., |
HARDWARE-IN-THE-LOOP INTEGRATED SIMULATION TECHNOLOGY FOR GAS TURBINES
AND ITS SYSTEMS |
ÒÅÕÍÎËÎÃ²ß ÍÀϲÂÍÀÒÓÐÍÎÃÎ ÊÎÌÏËÅÊÑÍÎÃÎ
ÌÎÄÅËÞÂÀÍÍß ÃÒÄ ² ÉÎÃÎ ÑÈÑÒÅÌ |
ÒÅÕÍÎËÎÃÈß
ÏÎËÓÍÀÒÓÐÍÎÃÎ ÊÎÌÏËÅÊÑÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß ÃÒÄ È ÅÃÎ ÑÈÑÒÅÌ |
172–180 |
Ïàí³í Â.Â., |
FORMATION OF THE STRUCTURE OF INTELLECTUAL AUTOMATIC CONTROL SYSTEM OF
GAS TURBINE ENGINES |
ÔÎÐÌÓÂÀÍÍß
ÑÒÐÓÊÒÓÐÈ ²ÍÒÅËÅÊÒÓÀËÜÍί ÑÈÑÒÅÌÈ ÀÂÒÎÌÀÒÈ×ÍÎÃÎ ÊÅÐÓÂÀÍÍß À²ÀÖ²ÉÍÈÌ ÃÒÄ |
ÔÎÐÌÈÐÎÂÀÍÈÅ ÑÒÐÓÊÒÓÐÛ ÈÍÒÅËËÅÊÒÓÀËÜÍÎÉ ÑÈÑÒÅÌÛ ÀÂÒÎÌÀÒÈ×ÅÑÊÎÃÎ ÓÏÐÀÂËÅÍÈß
ÀÂÈÀÖÈÎÍÍÛÌ ÃÒÄ |
181–185 |
Ñóâîðîâ Ì.À., |
AUTOMATION OF DESIGN PROCESS
OF AIRCRAFT ENGINE PARTS IN THE "VERTICAL" |
ÀÂÒÎÌÀÒÈÇÀÖ²ß ÏÐÎÖÅÑÓ
ÏÐÎÅÊÒÓÂÀÍÍß ÒÅÕÍÎËÎò×ÍÎÃÎ ÏÐÎÖÅÑÓ ÄÅÒÀ˲ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ  ÑÈÑÒÅ̲ «ÂÅÐÒÈÊÀËÜ» |
186–189 |
|
Äìèòð³ºâ Ñ.Î., |
AIRCRAFT
ENGINES MAINTENANCE PROGRAMS DEVELOPMENT |
ÔÎÐÌÓÂÀÍÍß ÏÐÎÃÐÀÌ
ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÔÎÐÌÈÐÎÂÀÍÈÅ
ÏÐÎÃÐÀÌÌ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
190–194 |
Òóðêèí È.Á., |
THE TECHNOLOGY
OF STANDARD PROFILE FORMATION WHICH SERVES TO CERTIFICATE THE SOFTWARE
SYSTEMS |
ÒÅÕÍÎËÎÃ²ß ÔÎÐÌÓÂÀÍÍß ÍÎÐÌÀÒÈÂÍÎÃÎ
ÏÐÎÔ²ËÞ ÄËß ÑÅÐÒÈÔ²ÊÖ²¯ ÏÐÎÃÐÀÌÍÈÕ ÑÈÑÒÅÌ |
ÒÅÕÍÎËÎÃÈß
ÔÎÐÌÈÐÎÂÀÍÈß ÍÎÐÌÀÒÈÂÍÎÃÎ ÏÐÎÔÈËß ÄËß ÑÅÐÒÈÔÈÊÀÖÈÈ ÏÐÎÃÐÀÌÌÍÛÕ ÑÈÑÒÅÌ |
195–199 |
×åõðåñàç Ì. |
FEATURES OF
BITANGETIAL TREATMENT OF DIFFICULT SURFACES OF DETAIL OF AVIATION ENGINE WITH
THE USE OF SOFTWARE TOPSOLID |
ÎÑÎÁËÈÂÎÑÒ² Á²ÒÀÍÃÅÖ²ÉÍί ÎÁÐÎÁÊÈ
ÑÊËÀÄÍÈÕ ÏÎÂÅÐÕÎÍÜ ÄÅÒÀ˲ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÏÐÎÃÐÀÌÍÎÃÎ ÇÀÁÅÇÏÅ×ÅÍÍß TOPSOLID |
200–205 |
|
Áóòåíêî Þ.È. |
THE GENERALIZED
MODEL OF THE KERNEL SEMANTIC INTEGRITY OF LANGUAGE OF STANDARDS OF THE
SOFTWARE |
ÓÇÀÃÀËÜÍÅÍÀ ÌÎÄÅËÜ ßÄÐÀ ÑÅÌÀÍÒÈ×Íί
ֲ˲ÑÍÎÑÒ² ÌÎÂÈ ÑÒÀÍÄÀÐҲ ÏÐÎÃÐÀÌÍÎÃÎ ÇÀÁÅÇÏÅ×ÅÍÍß |
ÎÁÎÁÙÅÍÍÀß ÌÎÄÅËÜ
ßÄÐÀ ÑÅÌÀÍÒÈ×ÅÑÊÎÉ ÖÅËÎÑÒÍÎÑÒÈ ßÇÛÊÀ ÑÒÀÍÄÀÐÒΠÏÐÎÃÐÀÌÌÍÎÃÎ ÎÁÅÑÏÅ×ÅÍÈß |
206–210 |
Êó÷óê Ã.À. |
METHOD OF THE
AGGREGATED TRAFFIC STATISTICAL
DESCRIPTIONS OPERATIVE ESTIMATION |
ÌÅÒÎÄ ÎÏÅÐÀÒÈÂÍί ÎÖ²ÍÊÈ ÑÒÀÒÈÑÒÈ×ÍÈÕ
ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÀÃÐÅÃÎÂÀÍÎÃÎ ÒÐÀÔ²ÊÀ |
ÌÅÒÎÄ ÎÏÅÐÀÒÈÂÍÎÉ
ÎÖÅÍÊÈ ÑÒÀÒÈÑÒÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÀÃÐÅÃÈÐÎÂÀÍÍÎÃÎ ÒÐÀÔÈÊÀ |
211–214 |
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè,
ïðîãðàììàìè è ïðîåêòàìè |
||||
Ðåâà À.Í., |
EFFICIENCY OF
THE ORGANIZATION COMMUNICATIONS IN A SYSTEM OF AERONAVIGATION SERVICE OF
FLIGHTS (ON THE EXAMPLE OF KRASNOYARSK AIR TRAFFIC SERVICE CENTER) |
ÅÔÅÊÒÈÂͲÑÒÜ
ÎÐÃÀͲÇÀÖ²¯ ÊÎÌÓͲÊÀÖ²É Â ÑÈÑÒÅ̲ ÀÅÐÎÍÀ²ÃÀÖ²ÉÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÏÎËÜÎÒ²Â
(ÍÀ ÏÐÈÊËÀIJ ÊÐÀÑÍÎßÐÑÜÊÎÃÎ ÖÅÍÒÐÓ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÐÓÕÓ) |
215–226 |
|
Äàíîâà Ì.À. |
METHODS OF SELECTION PRIORITIES FOR FORECASTING THE SCIENTIFIC AND
TECHNICAL DEVELOPMENT OF LARGE-SCALE OBJECTS ON THE BASIS OF TECHNOLOGY
FORESIGHT |
ÌÅÒÎÄÈÊÀ ÂÈÁÎÐÓ ÏвÎÐÈÒÅҲ ÏÐÈ ÏÐÎÃÍÎÇÓÂÀÍͲ ÍÀÓÊÎÂÎ-ÒÅÕͲ×ÍÎÃÎ
ÐÎÇÂÈÒÊÓ ÂÅËÈÊÎÌÀÑØÒÀÁÍÈÕ ÎÁ'ªÊҲ ÍÀ ÎÑÍβ ÒÅÕÍÎËÎò¯ ÔÎÐÑÀÉÒ |
227–231 |
|
Äåìüÿíåíêî Â.À. |
THE
KNOWLEDGE-ORIENTED METHOD OF SUPPORT OF DECISION-MAKING BY TECHNOLOGICAL
PREPARATION OF PRODUCTION OF CONSUMER GOODS AT MACHINE-BUILDING ENTERPRISE |
ÌÅÒÎÄ ÇÍÀÍÍßÎвªÍÒÎÂÀÍί ϲÄÒÐÈÌÊÈ
ÏÐÈÉÍßÒÒß Ð²ØÅÍÜ ÏÐÈ ÒÅÕÍÎËÎò×Í²É Ï²ÄÃÎÒÎÂÖ² ÂÈÐÎÁÍÈÖÒÂÀ ÒÎÂÀв ÍÀÐÎÄÍÎÃÎ
ÑÏÎÆÈÂÀÍÍß ÍÀ ÌÀØÈÍÎÁÓIJÂÍÎÌÓ Ï²ÄÏÐȪÌÑÒ² |
232–237 |
|
Ëþá÷åíêî Â.Â. |
PROCESSING OF INFORMATION MANAGEMENT SYSTEM INDUSTRIES |
ÎÁÐÎÁÊÀ ²ÍÔÎÐÌÀÖ²¯
 ÑÈÑÒÅ̲ ÊÅÐÓÂÀÍÍß ÏÐÎÌÈÑËÎÂÈÌ Ï²ÄÏÐȪÌÑÒÂÎÌ |
ÎÁÐÀÁÎÒÊÀ ÈÍÔÎÐÌÀÖÈÈ Â ÑÈÑÒÅÌÅ
ÓÏÐÀÂËÅÍÈß ÏÐÎÌÛØËÅÍÍÛÌ ÏÐÅÄÏÐÈßÒÈßÌ |
238–241 |
Ïîòàïîâà Ì. |
BUSINESS
PROCESS MANAGEMENT METHODS IN SOFTWARE FIRM ON THE BASIS OF UNDERDETERMINED
PRINCIPLE |
ÌÅÒÎÄÈÊÀ ÓÏÐÀÂ˲ÍÍß Á²ÇÍÅÑ-ÏÐÎÖÅÑÀÌÈ Â
ÑÎÔÒÂÅÐÍ²É Ô²Ð̲ ÍÀ ÎÑÍβ ÏÐÈÍÖÈÏÓ ÍÅÄÎÂÈÇÍÀ×ÅÍÎÑÒ² |
ÌÅÒÎÄÈÊÀ
ÓÏÐÀÂËÅÍÈß ÁÈÇÍÅÑ-ÏÐÎÖÅÑÑÀÌÈ Â ÑÎÔÒÂÅÐÍÎÉ ÔÈÐÌÅ ÍÀ ÎÑÍÎÂÅ ÏÐÈÍÖÈÏÀ
ÍÅÄÎÎÏÐÅÄÅËÅÍÍÎÑÒÈ |
242–246 |
Ñí³æíîé Ã.Â., |
CERTIFICATION
AND QUALITY OF AIRCRAFT ENTERPRISE |
ÑÅÐÒÈÔÈÊÀÖÈß È ÑÈÑÒÅÌÀ ÊÀ×ÅÑÒÂÀ
ÀÂÈÀÖÈÎÍÍÎÃÎ ÏÐÅÄÏÐÈßÒÈß |
247–250 |
|
Ñòåïàíåíêî Ñ.Ì. |
ITEMS OF
PROJECT MANAGEMENT STANDARTIZATION ACCORDING TO APU-21 AVIATION REGULATIONS |
ÏÈÒÀÍÍß CÒÀÍÄÀÐÒÈÇÀÖÈÈ ÓÏÐÀÂ˲ÍÍß
ÏÐÎÅÊÒÓÂÀÍÍßÌ Â²ÄÏβÄÍÎ ÄÎ À²ÀÖ²ÉÍÈÕ ÏÐÀÂÈË ÀÏÓ-21 |
ÂÎÏÐÎÑÛ
CÒÀÍÄÀÐÒÈÇÀÖÈÈ ÓÏÐÀÂËÅÍÈß ÏÐÎÅÊÒÈÐÎÂÀÍÈÅÌ Â ÑÎÎÒÂÅÒÑÒÂÈÈ Ñ ÀÂÈÀÖÈÎÍÍÛÌÈ
ÏÐÀÂÈËÀÌÈ ÀÏÓ-21 |
251–254 |
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.