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.
The Impact of Fuel Fluidity in Wing Tanks on the Aeroelasticity Characteristics of an Aircraft
Russ. Aeronaut.
Russian Aeronautics ; 65 , 4 ; 629-638
2022-10-01
10 pages
Article (Journal)
Electronic Resource
English
Structural Dynamics and Aeroelasticity of Rotary Wing Aircraft
British Library Conference Proceedings | 2000
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