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. J Comput Methods Eng. 2022;26(1):197-207 (In Persian).
