Abstract
This paper describes analysis of aerodynamic vibration of a square prism in two-dimensional flow,The simulation in conducted by means of New Hybrid Aerodynamic Vibration Technique.The analysis focuces the relation between the density ratio and oscillation velocity.The phenomenon of aerodynamic vibration in air flow depends on Scruton number that in formulated by the product of density ratio and damping parameter.However,the oscillation velocity is getting smaller with the density ratio getting smaller even though the Scruton numbers are similar.In this simulation,similar result was oftained,and the peak response frequency gets smaller than the natural frequency.