COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL
Efficiency of air-cushion chassis pitching moment control by nozzles rotation at take-off and landing condition of aircraft experimental research is carried out. Researches were conducted using double circuit air-cushion vehicle nozzle device with rotary sheets-nozzles at “flat cell” test bench. Dur...
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Moscow State Technical University of Civil Aviation
2016-11-01
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Series: | Naučnyj Vestnik MGTU GA |
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Online Access: | https://avia.mstuca.ru/jour/article/view/381 |
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doaj-b23b71bf6d5b45a9b77f2e4170d56ace2021-07-28T21:00:36ZrusMoscow State Technical University of Civil Aviation Naučnyj Vestnik MGTU GA2079-06192542-01192016-11-012119399381COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROLYu. Yu. Merzlikin0A. A. Dolgopolov1V. G. Cipenko2НИО-12 «Научно-исследовательского Московского комплекса ЦАГИ» «ФГУП» ЦАГИНИО-12 «Научно-исследовательского Московского комплекса ЦАГИ» «ФГУП» ЦАГИМГТУ ГАEfficiency of air-cushion chassis pitching moment control by nozzles rotation at take-off and landing condition of aircraft experimental research is carried out. Researches were conducted using double circuit air-cushion vehicle nozzle device with rotary sheets-nozzles at “flat cell” test bench. During the experiment parameters, such as: incident flow speed V, pressure at receiver Pp, height of model above the plane h, angle of pitch υ, nozzle mounting angles QUOTE , QUOTE were varied.https://avia.mstuca.ru/jour/article/view/381управлениепродольный моментлетательный аппаратшассивоздушная подушка |
collection |
DOAJ |
language |
Russian |
format |
Article |
sources |
DOAJ |
author |
Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko |
spellingShingle |
Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL Naučnyj Vestnik MGTU GA управление продольный момент летательный аппарат шасси воздушная подушка |
author_facet |
Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko |
author_sort |
Yu. Yu. Merzlikin |
title |
COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
title_short |
COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
title_full |
COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
title_fullStr |
COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
title_full_unstemmed |
COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
title_sort |
composite circuit aircraft with air-cushion chassis pitching moment control |
publisher |
Moscow State Technical University of Civil Aviation |
series |
Naučnyj Vestnik MGTU GA |
issn |
2079-0619 2542-0119 |
publishDate |
2016-11-01 |
description |
Efficiency of air-cushion chassis pitching moment control by nozzles rotation at take-off and landing condition of aircraft experimental research is carried out. Researches were conducted using double circuit air-cushion vehicle nozzle device with rotary sheets-nozzles at “flat cell” test bench. During the experiment parameters, such as: incident flow speed V, pressure at receiver Pp, height of model above the plane h, angle of pitch υ, nozzle mounting angles QUOTE , QUOTE were varied. |
topic |
управление продольный момент летательный аппарат шасси воздушная подушка |
url |
https://avia.mstuca.ru/jour/article/view/381 |
work_keys_str_mv |
AT yuyumerzlikin compositecircuitaircraftwithaircushionchassispitchingmomentcontrol AT aadolgopolov compositecircuitaircraftwithaircushionchassispitchingmomentcontrol AT vgcipenko compositecircuitaircraftwithaircushionchassispitchingmomentcontrol |
_version_ |
1721263738582990848 |