Consider two different flows over geometrically similar airfoil shapes, one airfoil being twice the size of the other. The flow over the smaller airfoil has free stream properties given by T_∞ = 200 K., p_∞ = 1.23 kg/m³, and V_∞= 100 m/s. The flow over the larger airfoil is described by T_∞ = 800K, p_∞ = 1.739 kg/m³, and V_∞ = 200rn/s. Assume that both μ and a are proportional to T^1/2. Are the two flows dynamically similar?