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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| Format: | Article |
| Language: | Russian |
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Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Научный вестник МГТУ ГА |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/381 |
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| _version_ | 1849252708095098880 |
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| author | Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko |
| author_facet | Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko |
| author_sort | Yu. Yu. Merzlikin |
| collection | DOAJ |
| 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. |
| format | Article |
| id | doaj-art-b23b71bf6d5b45a9b77f2e4170d56ace |
| institution | Kabale University |
| issn | 2079-0619 2542-0119 |
| language | Russian |
| publishDate | 2016-11-01 |
| publisher | Moscow State Technical University of Civil Aviation |
| record_format | Article |
| series | Научный вестник МГТУ ГА |
| spelling | doaj-art-b23b71bf6d5b45a9b77f2e4170d56ace2025-08-20T03:56:33ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-012119399381COMPOSITE 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/381controlpitching momentaircraftlanding gearair cushion |
| spellingShingle | Yu. Yu. Merzlikin A. A. Dolgopolov V. G. Cipenko COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL Научный вестник МГТУ ГА control pitching moment aircraft landing gear air cushion |
| title | 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_short | COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL |
| title_sort | composite circuit aircraft with air cushion chassis pitching moment control |
| topic | control pitching moment aircraft landing gear air cushion |
| url | https://avia.mstuca.ru/jour/article/view/381 |
| work_keys_str_mv | AT yuyumerzlikin compositecircuitaircraftwithaircushionchassispitchingmomentcontrol AT aadolgopolov compositecircuitaircraftwithaircushionchassispitchingmomentcontrol AT vgcipenko compositecircuitaircraftwithaircushionchassispitchingmomentcontrol |