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
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Ìàêàåâà Ð.Õ.,
Êàðèìîâ À.Õ.,
Öàðåâà À.Ì.

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
(
5)

Ãóñàðåâ Â.Ñ.,
ßðîâîé Þ.Â.

Experimental study of dependence of technological system action of form-building modes

åêñïåð³ìåíòàëüíå äîñë³äæåííÿ çàëåæíîñò³ 䳿 òåõíîëîã³÷íî¿ ñèñòåìè â³ä ðåæèì³â ôîðìîóòâîðåííÿ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÇÀÂÈÑÈÌÎÑÒÈ ÄÅÉÑÒÂÈß ÒÅÕÍÎËÎÃÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ ÎÒ ÐÅÆÈÌΠÔÎÐÌÎÎÁÐÀÇÎÂÀÍÈß

12–16
(
5)

Êàëèíèíà Í.Å.,
Êàëèíîâñêàÿ À.Å.,
Êàëèíèí Â.Ò.

MATERIAL SCIENCE ASPECTS OF NANOMODIFICATION MULTICOMPONENT NICKEL ALLOYS

ÌÀÒÅвÀËÎÇÍÀÂײ ÀÑÏÅÊÒÈ ÍÀÍÎÌÎÄÈÔ²ÊÓÂÀÍÍß ÁÀÃÀÒÎÊÎÌÏÎÍÅÍÒÍÈÕ Í²ÊÅËÅÂÈÕ ÑÏËÀ²Â

ÌÀÒÅÐÈÀËÎÂÅÄ×ÅÑÊÈÅ ÀÑÏÅÊÒÛ ÍÀÍÎÌÎÄÈÔÈÖÈÐÎÂÀÍÈß ÌÍÎÃÎÊÎÌÏÎÍÅÍÒÍÛÕ ÍÈÊÅËÅÂÛÕ ÑÏËÀÂÎÂ

17–21
(
5)

Ìîçãîâîé Â.Ô.,
Áàëóøîê Ê.Á.,
Êîòîâ È.È.,
Ïàíàñåíêî Â.À.,
Áèðóê Ì.Ê.

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
(
7)

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

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 ÑÏËÀ²Â

ÑÊÎÐÎÑÒÜ ÐÅÇÊÈ ÐÀÇÓÏÐÎ×ÍÅÍÈÅÌ ÑÂÅÐÕÇÂÓÊÎÂÛÌÈ ÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÛÌÈ ÃÀÇÎÂÛÌÈ ÑÒÐÓßÌÈ ÌÀÒÅÐÈÀËΠÍÀ ÎÑÍÎÂÅ ÀËÞÌÈÍÈÅÂÛÕ ÑÏËÀÂÎÂ

29–32
(
4)

Ñîðîêèí Â.Ô.,
Áóò Ò.Ï.,
Êîìáàðîâ Â.Â.

SYNTHESIS OF INVOLUTE PATHS OF HIGH-SPEED MACHINING OF HOLES

ÑÈÍÒÅÇ ÅÂÎËÜÂÅÍÒÍÈÕ ÒÐÀªÊÒÎÐ²É ÂÈÑÎÊÎØÂÈÄʲÑÍÎÃÎ ÔÐÅÇÅÐÓÂÀÍÍß ÎÒÂÎвÂ

ÑÈÍÒÅÇ ÝÂÎËÜÂÅÍÒÍÛÕ ÒÐÀÅÊÒÎÐÈÉ ÂÛÑÎÊÎÑÊÎÐÎÑÒÍÎÉ ÐÀÑÔÐÅÇÅÐÎÂÊÈ ÎÒÂÅÐÑÒÈÉ

33–38
(
6)

Áûáèí À.À.,
Íåâüÿíöåâà Ð.Ð.,
Ñìûñëîâ À.Ì.,
Ñìîëüíèêîâà Î.Ã.

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
(
4)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ðîäèòåëåâ Â.È.,
Íåñòåðåíêî Â.Ã.

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
(
10)

Ñîðî÷êèí À.Í.,
Ëîãèíîâ Â.Â.,
Åëàíñêèé À.Â.

ANALYSIS OF WAYS TO CARRY OUT MODERNIZATION OF ATTACK AIRCRAFT SU-25 IN ORDER TO IMPROVE ITS OPERATING PERFORMANCE

ÀÍÀË²Ç ØËßղ ÌÎÄÅÐͲÇÀÖ²¯ ˲ÒÀÊÀ ØÒÓÐÌÎÂÈÊÀ ÒÈÏÓ ÑÓ-25 Ç ÌÅÒÎÞ ÏÎÊÐÀÙÅÍÍß ÉÎÃÎ ÅÊÑÏËÓÀÒÀÖ²ÉÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ

ÀÍÀËÈÇ ÏÓÒÅÉ ÌÎÄÅÐÍÈÇÀÖÈÈ ÑÀÌÎËÅÒÀ ØÒÓÐÌÎÂÈÊÀ ÒÈÏÀ ÑÓ-25 Ñ ÖÅËÜÞ ÓËÓרÅÍÈß ÅÃÎ ÝÊÑÏËÓÀÒÀÖÈÎÍÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ

53–60
(
8)

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
(
6)

Ìîãèëüíèêîâ Â.Ï.,
Èîíîâ À.Â.

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

ÌÅÒÎÄÈÊÈ Ë¨ÒÍÛÕ ÈÑÏÛÒÀÍÈÉ ×ÈÑÒÎÒÛ ÂÎÇÄÓÕÀ, ÎÒÁÈÐÀÅÌÎÃÎ ÎÒ ÀÂÈÀÖÈÎÍÍÛÕ ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÍÓÆÄÛ ÑÈÑÒÅÌ ÊÎÍÄÈÖÈÎÍÈÐÎÂÀÍÈß ÂÎÇÄÓØÍÛÕ ÑÓÄÎÂ

67–72
(
6)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Ãèðüêà Þ.Â.,
Ãàíãàí È.À.,
Êðàøàíèöà Þ.À.

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
(
5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Àë¸õèí Ñ.À.,
Ïîïîâ Ã.Ê.

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
(
5)

Êèñëîâ Î.Â.

THE GAS TURBINE ENGINE GAS GENERATOR CHARACTERISTICS

ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÃÒÄ

ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀ ÃÒÄ

83–86
(
4)

Õàëàòîâ À.À.,
Áåçëþäíàÿ Ì.Â.,
Äàøåâñêèé Þ.ß.,
Ñåâåðèí Ñ.Ä.,
Áîðèñîâ È.È.

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

ÀÄÀÏÒÀÖÈß k-ε ÌÎÄÅËÈ ÒÓÐÁÓËÅÍÒÍÎÑÒÈ ÄËß ÌÎÄÅËÈÐÎÂÀÍÈß ÏËÅÍÎ×ÍÎÃÎ ÎÕËÀÆÄÅÍÈß ×ÅÐÅÇ ÑÈÑÒÅÌÓ ÄÂÓÕÐßÄÍÛÕ ÎÒÂÅÐÑÒÈÉ Â ÑÔÅÐÈ×ÅÑÊÈÕ ÓÃËÓÁËÅÍÈßÕ

87–91
(
5)

Äîëìàòîâ Ä.À.,
Êóêóðóäçà À.Â.

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
(
5)

Êðàâ÷åíêî È.Ô.,
Õîìûëåâ Ñ.À.,
Âàðâàðóê Ï.Ï.,
Ïèêà Å.Ë.

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
(
6)

Âàñèëüåâ È.Ï.,
Ïàâëîâà Ì.Â.,
Øåïåëü Â.Ò.

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
(
4)

Ãóñåâ Þ.À.,
Êîíîíûõèí Å.À.,
Êàõðàè Êàìáèç

RESISTIVE-STRAIN SENSORS WITH BYPASSING-PROTECTION SCREEN

ÒÅÍÇÎÐÅÇÈÑÒÎÐÈ Ç ÀÍÒ²ØÓÍÒÓÞ×ÈÌ ÅÊÐÀÍÎÌ

ÒÅÍÇÎÐÅÇÈÑÒÎÐÛ Ñ ÀÍÒÈØÓÍÒÈÐÓÞÙÈÌ ÝÊÐÀÍÎÌ

107–111
(
5)

Ëîÿí À.Â.,
Òèòîâ Ì.Þ.,
Ñîëîíèíêî Å.Ï.

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 ÊÀÒÎIJ ÅÐÄ

ÐÀÑ×ÅÒÍÛÉ ÑÏÎÑÎÁ ÎÏÐÅÄÅËÅÍÈß ÝÔÔÅÊÒÈÂÍÎÉ ÒÅÏËÎÏÐÎÂÎÄÍÎÑÒÈ ÌÅÒÀËËÎÏÎÐÈÑÒÛÕ ÝÌÈÒÒÅÐΠÊÀÒÎÄΠÝÐÄ

112–116
(
5)

Íåñòåðåíêî Ñ.Þ.,
Ðîøàíïóð Ø.

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 ²ÎͲÂ

ÑÈÑÒÅÌÀ ÓÐÀÂÍÅÍÈÉ ÌÎÌÅÍÒΠÔÓÍÊÖÈÈ ÐÀÑÏÐÅÄÅËÅÍÈß ×ÀÑÒÈÖ ÏÎ ÑÊÎÐÎÑÒßÌ Â ÐÀÇÐÅÆÅÍÍÎÉ ÑÐÅÄÅ ÈÍÄÓÊÖÈÎÍÍÛÕ ÈÑÒÎ×ÍÈÊΠÏËÀÇÌÛ, ÝËÅÊÒÐÎÍÎÂ È ÈÎÍÎÂ

117–120
(
4)

Ãîëîùàïîâ Â.Í.,
Àíòèïöåâ Þ.Ï.,
Êîòóëüñêàÿ Î.Â.,
Ïàðàìîíîâà Ò.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
(
6)

Ðàä÷åíêî Ð.Í.,
Ñòàõåëü À.,
Ðàä÷åíêî Í.È.,
Ñèðîòà À.À.

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
(
6)

Ñèí÷åíêî Ñ.Â.,
Øèðèíñêèé 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

ÏÎÑÒÐÎÅÍÈÅ ÌÀÒÅÌÀÒÈ×ÅÑÊÈÕ ÌÎÄÅËÅÉ ÐÀÇÐßÄÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÝËÅÊÒÐÎÕÈÌÈ×ÅÑÊÈÕ ÀÊÊÓÌÓËßÒÎÐΠÐÀÇËÈ×ÍÛÕ ÒÈÏΠÏÐÈ ÏÎÌÎÙÈ ÑÕÅÌ ÇÀÌÅÙÅÍÈß

133–138
(
6)

Äçåíçåðñêèé Â.À.,
Êàçà÷à Þ.È.,
Æóëàé Þ.À.,
Èâàíîâ Â.À.,
Ñêîñàðü Â.Þ.

DEVELOPMENT OF NEW TECHNOLOGIES IMPROVE THE MECHANICAL PROPERTIES OF BATTERY LEAD ALLOYS

ÐÎÇÐÎÁÊÀ ÍÎÂÈÕ ÒÅÕÍÎËÎÃ²É Ï²ÄÂÈÙÅÍÍß ÌÅÕÀͲ×ÍÈÕ ÂËÀÑÒÈÂÎÑÒÅÉ ÑÂÈÍÖÅÂÈÕ ÑÏËÀ² ÄËß ÀÊÓÌÓËßÒÎвÂ

ÐÀÇÐÀÁÎÒÊÀ ÍÎÂÛÕ ÒÅÕÍÎËÎÃÈÉ ÏÎÂÛØÅÍÈß ÌÅÕÀÍÈ×ÅÑÊÈÕ ÑÂÎÉÑÒ ÑÂÈÍÖÎÂÛÕ ÑÏËÀÂΠÄËß ÀÊÊÓÌÓËßÒÎÐÎÂ

139–143
(
5)

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
(
7)

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
(
6)

Øåïåòîâ Þ.À.,
Äîëæèêîâà Å.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˲

ÌÎÄÅËÈÐÎÂÀÍÈÅ ÝÍÅÐÃÎÏÐÈÕÎÄÀ ÎÒ ÑÎËÍÅ×ÍÛÕ ÁÀÒÀÐÅÉ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÀÏÏÀÐÀÒÀ ÊËÀÑÑÀ ÌÈÊÐÎÑÏÓÒÍÈÊ ÄËß ÄÈÑÒÀÍÖÈÎÍÍÎÃÎ ÇÎÍÄÈÐÎÂÀÍÈß ÇÅÌËÈ

157–160
(
4)

Ðÿáêîâ Â.È.,
Òîëìà÷åâ Í.Ã.

ENERGETIC CONDITIONS OF "COLD" FUSION

ÒÀÕ²ÎÍÍÀ ÅÍÅÐÃ²ß – ÎÑÍÎÂÀ «ÕÎËÎÄÍÎÃλ ÑÈÍÒÅÇÓ

ÒÀÕÈÎÍÍÀß ÝÍÅÐÃÈß – ÎÑÍÎÂÀ «ÕÎËÎÄÍÎÃλ ÑÈÍÒÅÇÀ

161–167
(
7)

Äàíîâ À.Ñ.

FUNDUMENTAL ENERGY LEVELS OF MATTER

ÔÓÍÄÀÌÅÍÒÀËÜͲ ÅÍÅÐÃÅÒÈ×Ͳ вÂͲ ÌÀÒÅв¯

ÔÓÍÄÀÌÅÍÒÀËÜÍÛÅ ÝÍÅÐÃÅÒÈ×ÅÑÊÈÅ ÓÐÎÂÍÈ ÌÀÒÅÐÈÈ

168–171
(
4)

Èíôîðìàöèîííûå òåõíîëîãèè

Ïîãîðåëîâ Ã.È.,
Àáäóëíàãèìîâ À.È.,
Ãîäîâàíþê À.Ã.

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
(
9)

Ïàí³í Â.Â.,
ªí÷åâ Ñ.Â.,
Òàêó Ñ.Î.

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
(
5)

Ñóâîðîâ Ì.À.,
Òðåòüÿê Â.Â.,
Ñîòíèêîâ Â.Ä.,
Õóäÿêîâ Ñ.Â.

AUTOMATION OF DESIGN PROCESS OF AIRCRAFT ENGINE PARTS IN THE "VERTICAL"

ÀÂÒÎÌÀÒÈÇÀÖ²ß ÏÐÎÖÅÑÓ ÏÐÎÅÊÒÓÂÀÍÍß ÒÅÕÍÎËÎò×ÍÎÃÎ ÏÐÎÖÅÑÓ ÄÅÒÀ˲ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ  ÑÈÑÒÅ̲ «ÂÅÐÒÈÊÀËÜ»

ÀÂÒÎÌÀÒÈÇÀÖÈß ÏÐÎÖÅÑÑÀ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÒÅÕÍÎËÎÃÈÈ ÈÇÃÎÒÎÂËÅÍÈß ÄÅÒÀËÈ ÊÎÐÏÓÑÀ ÐÅÃÓËßÒÎÐÀ Â ÑÈÑÒÅÌÅ «ÂÅÐÒÈÊÀËÜ»

186–189
(
4)

Äìèòð³ºâ Ñ.Î.,
Áóðëàêîâ Â.².,
Ïîïîâ Î.Â.,
Ïîïîâ Ä.Â.

AIRCRAFT ENGINES MAINTENANCE PROGRAMS DEVELOPMENT

ÔÎÐÌÓÂÀÍÍß ÏÐÎÃÐÀÌ ÒÅÕͲ×ÍÎÃÎ ÎÁÑËÓÃÎÂÓÂÀÍÍß À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲÂ

ÔÎÐÌÈÐÎÂÀÍÈÅ ÏÐÎÃÐÀÌÌ ÒÅÕÍÈ×ÅÑÊÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ

190–194
(
5)

Òóðêèí È.Á.,
Ñòàðèêîâ Ñ.Í.,
Øîñòàê È.Â.

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
(
5)

×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

ÎÑÎÁÅÍÍÎÑÒÈ ÁÈÒÀÍÃÅÖÈÀËÜÍÎÉ ÎÁÐÀÁÎÒÊÈ ÑËÎÆÍÛÕ ÏÎÂÅÐÕÍÎÑÒÅÉ ÄÅÒÀËÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß  Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÏÐÎÃÐÀÌÌÍÎÃÎ ÎÁÅÑÏÅ×ÅÍÈß TOPSOLID

200–205
(
6)

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
(
5)

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
(4)

Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè

Ðåâà À.Í.,
Óñòèìåíêî È.Ì.,
Êîëòàêîâ Â.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 ÏÎËÜÎҲ (ÍÀ ÏÐÈÊËÀIJ ÊÐÀÑÍÎßÐÑÜÊÎÃÎ ÖÅÍÒÐÓ ÎÁÑËÓÃÎÂÓÂÀÍÍß ÏβÒÐßÍÎÃÎ ÐÓÕÓ)

ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÎÐÃÀÍÈÇÀÖÈÈ ÊÎÌÌÓÍÈÊÀÖÈÉ Â ÑÈÑÒÅÌÅ ÀÝÐÎÍÀÂÈÃÀÖÈÎÍÍÎÃÎ ÎÁÑËÓÆÈÂÀÍÈß ÏÎËÅÒΠ(ÍÀ ÏÐÈÌÅÐÅ ÊÐÀÑÍÎßÐÑÊÎÃÎ ÖÅÍÒÐÀ ÎÁÑËÓÆÈÂÀÍÈß ÂÎÇÄÓØÍÎÃÎ ÄÂÈÆÅÍÈß)

215–226
(
12)

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

ÌÅÒÎÄÈÊÀ ÂÛÁÎÐÀ ÏÐÈÎÐÈÒÅÒΠÏÐÈ ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÈ ÍÀÓ×ÍÎ-ÒÅÕÍÈ×ÅÑÊÎÃÎ ÐÀÇÂÈÒÈß ÊÐÓÏÍÎÌÀÑØÒÀÁÍÛÕ ÎÁÚÅÊÒΠÍÀ ÎÑÍÎÂÅ ÒÅÕÍÎËÎÃÈÈ ÔÎÐÑÀÉÒ

227–231
(
5)

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

ÌÅÒÎÄ ÇÍÀÍÈÅÎÐÈÅÍÒÈÐÎÂÀÍÍÎÉ ÏÎÄÄÅÐÆÊÈ ÏÐÈÍßÒÈß ÐÅØÅÍÈÉ ÏÐÈ ÒÅÕÍÎËÎÃÈ×ÅÑÊÎÉ ÏÎÄÃÎÒÎÂÊÅ ÏÐÎÈÇÂÎÄÑÒÂÀ ÒÎÂÀÐΠÍÀÐÎÄÍÎÃÎ ÏÎÒÐÅÁËÅÍÈß ÍÀ ÌÀØÈÍÎÑÒÐÎÈÒÅËÜÍÎÌ ÏÐÅÄÏÐÈßÒÈÈ

232–237
(
6)

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
(
4)

Ïîòàïîâà Ì.Â

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
(
5)

Ñí³æíîé Ã.Â.,
Òîìàøåâñüêèé Î.Â.,
Òåðüîøèíà Â.Ñ.

CERTIFICATION AND QUALITY OF AIRCRAFT ENTERPRISE

ÑÅÐÒÈÔ²ÊÀÖ²ß ² ÑÈÑÒÅÌÀ ßÊÎÑÒ² À²ÀÖ²ÉÍÎÃΠϲÄÏÐȪÌÑÒÂÀ

ÑÅÐÒÈÔÈÊÀÖÈß È ÑÈÑÒÅÌÀ ÊÀ×ÅÑÒÂÀ ÀÂÈÀÖÈÎÍÍÎÃÎ ÏÐÅÄÏÐÈßÒÈß

247–250
(
4)

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
(
4)

 

 

 

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.