The present invention provides a system for numerical simulation and test verification of icing characteristics of an aerostat, including: an aerostat icing characteristic calculation model and an aerostat icing characteristic test system. The aerostat icing characteristic calculation model is configured to obtain icing data of the aerostat through numerical simulation, and the aerostat icing characteristic test system is configured to obtain icing characteristic data of the aerostat through a physical simulation test. The calculation result obtained through the numerical simulation and the test result obtained through the physical simulation test are mutually verified and improved, so as to facilitate the in-depth research and accurate analysis of the icing characteristics of the aerostat.


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    Title :

    AEROSTAT ICING CHARACTERISTIC NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION SYSTEM


    Additional title:

    SYSTEM ZUR NUMERISCHEN SIMULATION UND EXPERIMENTELLEN VERIFIZIERUNG VON AEROSTATVEREISUNGSEIGENSCHAFTEN
    SIMULATION NUMÉRIQUE DE CARACTÉRISTIQUES DE GIVRAGE D'AÉROSTAT ET SYSTÈME DE VÉRIFICATION EXPÉRIMENTALE


    Contributors:
    LIU QIANG (author) / YANG YANCHU (author) / CUI YANXIANG (author) / CAI JINGJING (author) / ZHU RONGCHEN (author) / ZHAO KAIBIN (author)

    Publication date :

    2022-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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