COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL

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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Bibliographic Details
Main Authors: Yu. Yu. Merzlikin, A. A. Dolgopolov, V. G. Cipenko
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
управление
продольный момент
летательный аппарат
шасси
воздушная подушка
Online Access:https://avia.mstuca.ru/jour/article/view/381
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spelling 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
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