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...
Guardat en:
| Autors principals: | , , |
|---|---|
| Format: | Artigo |
| Idioma: | Russo |
| Publicat: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
| Col·lecció: | Научный вестник МГТУ ГА |
| Matèries: | |
| Accés en línia: | https://avia.mstuca.ru/jour/article/view/381 |
| Etiquetes: |
Sense etiquetes, Sigues el primer a etiquetar aquest registre!
|