In this paper, the equation of motion of an elastic 2 DoF wing model has been derived using Lagrange's 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 B. Ghadiri, (2022). Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects. Journal of Advanced Materials in Engineering (Esteghlal), 26(1), 197-207.
MLA
R. Ghasemi Asl; and B. Ghadiri. "Determination of Dynamic Instability Speed of an Unsweep Wing in Subsonic Flow Including Compressibility Effects", Journal of Advanced Materials in Engineering (Esteghlal), 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 Advanced Materials in Engineering (Esteghlal), 26(1), pp. 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 Advanced Materials in Engineering (Esteghlal), 2022; 26(1): 197-207.
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