PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT

The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic,...
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Autor*in:	V. P. Morozov [verfasserIn] A. V. Petrov [verfasserIn] Yu. Yu. Merzlikin [verfasserIn]

Format:	E-Artikel
Sprache:	Russisch

Erschienen:	2016

Schlagwörter:	самолет шасси на воздушной подушке компоновка согласование

Übergeordnetes Werk:	In: Научный вестник МГТУ ГА - Moscow State Technical University of Civil Aviation, 2017, (2016), 211, Seite 109-115
Übergeordnetes Werk:	year:2016 ; number:211 ; pages:109-115

Links:	Link aufrufen Link aufrufen Journal toc Journal toc

Katalog-ID:	DOAJ029969549

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allfields	(DE-627)DOAJ029969549 (DE-599)DOAJ05ebba8197a446109d14010abd89c219 DE-627 ger DE-627 rakwb rus TL1-4050 V. P. Morozov verfasserin aut PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws. самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics A. V. Petrov verfasserin aut Yu. Yu. Merzlikin verfasserin aut In Научный вестник МГТУ ГА Moscow State Technical University of Civil Aviation, 2017 (2016), 211, Seite 109-115 (DE-627)1015069045 25420119 nnns year:2016 number:211 pages:109-115 https://doaj.org/article/05ebba8197a446109d14010abd89c219 kostenfrei https://avia.mstuca.ru/jour/article/view/383 kostenfrei https://doaj.org/toc/2079-0619 Journal toc kostenfrei https://doaj.org/toc/2542-0119 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2016 211 109-115
spelling	(DE-627)DOAJ029969549 (DE-599)DOAJ05ebba8197a446109d14010abd89c219 DE-627 ger DE-627 rakwb rus TL1-4050 V. P. Morozov verfasserin aut PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws. самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics A. V. Petrov verfasserin aut Yu. Yu. Merzlikin verfasserin aut In Научный вестник МГТУ ГА Moscow State Technical University of Civil Aviation, 2017 (2016), 211, Seite 109-115 (DE-627)1015069045 25420119 nnns year:2016 number:211 pages:109-115 https://doaj.org/article/05ebba8197a446109d14010abd89c219 kostenfrei https://avia.mstuca.ru/jour/article/view/383 kostenfrei https://doaj.org/toc/2079-0619 Journal toc kostenfrei https://doaj.org/toc/2542-0119 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2016 211 109-115
allfields_unstemmed	(DE-627)DOAJ029969549 (DE-599)DOAJ05ebba8197a446109d14010abd89c219 DE-627 ger DE-627 rakwb rus TL1-4050 V. P. Morozov verfasserin aut PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws. самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics A. V. Petrov verfasserin aut Yu. Yu. Merzlikin verfasserin aut In Научный вестник МГТУ ГА Moscow State Technical University of Civil Aviation, 2017 (2016), 211, Seite 109-115 (DE-627)1015069045 25420119 nnns year:2016 number:211 pages:109-115 https://doaj.org/article/05ebba8197a446109d14010abd89c219 kostenfrei https://avia.mstuca.ru/jour/article/view/383 kostenfrei https://doaj.org/toc/2079-0619 Journal toc kostenfrei https://doaj.org/toc/2542-0119 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2016 211 109-115
allfieldsGer	(DE-627)DOAJ029969549 (DE-599)DOAJ05ebba8197a446109d14010abd89c219 DE-627 ger DE-627 rakwb rus TL1-4050 V. P. Morozov verfasserin aut PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws. самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics A. V. Petrov verfasserin aut Yu. Yu. Merzlikin verfasserin aut In Научный вестник МГТУ ГА Moscow State Technical University of Civil Aviation, 2017 (2016), 211, Seite 109-115 (DE-627)1015069045 25420119 nnns year:2016 number:211 pages:109-115 https://doaj.org/article/05ebba8197a446109d14010abd89c219 kostenfrei https://avia.mstuca.ru/jour/article/view/383 kostenfrei https://doaj.org/toc/2079-0619 Journal toc kostenfrei https://doaj.org/toc/2542-0119 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2016 211 109-115
allfieldsSound	(DE-627)DOAJ029969549 (DE-599)DOAJ05ebba8197a446109d14010abd89c219 DE-627 ger DE-627 rakwb rus TL1-4050 V. P. Morozov verfasserin aut PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT 2016 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws. самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics A. V. Petrov verfasserin aut Yu. Yu. Merzlikin verfasserin aut In Научный вестник МГТУ ГА Moscow State Technical University of Civil Aviation, 2017 (2016), 211, Seite 109-115 (DE-627)1015069045 25420119 nnns year:2016 number:211 pages:109-115 https://doaj.org/article/05ebba8197a446109d14010abd89c219 kostenfrei https://avia.mstuca.ru/jour/article/view/383 kostenfrei https://doaj.org/toc/2079-0619 Journal toc kostenfrei https://doaj.org/toc/2542-0119 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2016 211 109-115
language	Russian
source	In Научный вестник МГТУ ГА (2016), 211, Seite 109-115 year:2016 number:211 pages:109-115
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topic_facet	самолет шасси на воздушной подушке компоновка согласование Motor vehicles. Aeronautics. Astronautics
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author	V. P. Morozov
spellingShingle	V. P. Morozov misc TL1-4050 misc самолет misc шасси на воздушной подушке misc компоновка misc согласование misc Motor vehicles. Aeronautics. Astronautics PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT
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title	PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT
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title_auth	PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT
abstract	The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws.
abstractGer	The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws.
abstract_unstemmed	The principle of "early matching" aircraft aerohydrodynamic layouts with air cushion landing gear is suggested. Application of this principle is considered as an example of adaptation to the ball screw base circuit of light transport aircraft. The principle, other than weight, aerodynamic, technological and operational requirements includes additional project activities related to the installation of ball screws.
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title_short	PRINCIPLE "EARLY MATCHING" AERODYNAMIC DESIGN AIRCRAFT WITH LANDING GEAR HOVERCRAFT
url	https://doaj.org/article/05ebba8197a446109d14010abd89c219 https://avia.mstuca.ru/jour/article/view/383 https://doaj.org/toc/2079-0619 https://doaj.org/toc/2542-0119
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