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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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Principais autores: Yu. Yu. Merzlikin, A. A. Dolgopolov, V. G. Cipenko
Format: Artigo
Sprog:Russo
Udgivet: Moscow State Technical University of Civil Aviation 2016-11-01
Serier:Научный вестник МГТУ ГА
Fag:
control
pitching moment
aircraft
landing gear
air cushion
Online adgang:https://avia.mstuca.ru/jour/article/view/381
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