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.


    Access

    Download


    Export, share and cite



    Title :

    COMPOSITE CIRCUIT AIRCRAFT WITH AIR-CUSHION CHASSIS PITCHING MOMENT CONTROL


    Contributors:


    Publication date :

    2016



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    AIR CUSHION CHASSIS WITH MULTI-SECTION FORMATION FOR AIRCRAFT

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

    Free access

    Anti-pitching vehicle chassis structure

    MEI LEI / WANG DA / XIAO FENG et al. | European Patent Office | 2023

    Free access