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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL


    Beteiligte:
    Yu. Yu. Merzlikin (Autor:in) / A. A. Dolgopolov (Autor:in) / V. G. Cipenko (Autor:in)


    Erscheinungsdatum :

    2016



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    AIR CUSHION CHASSIS WITH MULTI-SECTION FORMATION FOR AIRCRAFT

    Y. Y. Merzlikin / A. A. Dolgopolov | DOAJ | 2016

    Freier Zugriff

    Anti-pitching vehicle chassis structure

    MEI LEI / WANG DA / XIAO FENG et al. | Europäisches Patentamt | 2023

    Freier Zugriff