A mathematical model is proposed that provides the calculation of aircraft aeroelasticity characteristics taking into account the fluidity of the fuel in the aircraft wing tanks. This paper demonstrates the results of using the mathematical model developed in terms of the An-124 aircraft.


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    Title :

    The Impact of Fuel Fluidity in Wing Tanks on the Aeroelasticity Characteristics of an Aircraft


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 65 , 4 ; 629-638


    Publication date :

    2022-10-01


    Size :

    10 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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