In this paper, the equation of motion of an elastic 2 DoF wing model has been derived using Lagranges method. The aerodynamic loads on the wing were calculated via the Strip-Theory and the effect of compressibility was included. Wing deflections due to bending and twist motions were determined using the Assume-Mode method. The aeroelastic equations were solved numerically using the V-g method. The results obtained for different types of wings were in good agreement with experimental data.
R. Ghasemi Asl, and and B. Ghadiri, (2022). Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects. Journal of Computational Methods in Engineering, 26(1), 197-207.
MLA
R. Ghasemi Asl, , and and B. Ghadiri, . "Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects", Journal of Computational Methods in Engineering, 26, 1, 2022, 197-207.
HARVARD
R. Ghasemi Asl, , and B. Ghadiri, (2022). 'Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects', Journal of Computational Methods in Engineering, 26(1), pp. 197-207.
CHICAGO
R. Ghasemi Asl and and B. Ghadiri, "Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects," Journal of Computational Methods in Engineering, 26 1 (2022): 197-207,
VANCOUVER
R. Ghasemi Asl, , and B. Ghadiri, Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects. Journal of Computational Methods in Engineering, 2022; 26(1): 197-207.
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