COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL

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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:	Научный вестник МГТУ ГА
Subjects:	control pitching moment aircraft landing gear air cushion
Online Access:	https://avia.mstuca.ru/jour/article/view/381
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