“…As ε → 0, the limit of solutions of (1.3) is called the low Mach limit [16,17]. Similar to [1,13,26], we assume that the pressure is a small perturbation of a given constant stateP > 0, i.e. P =P + O(ε), (1.4) and without loss of generality, we further assumeP to be 1.…”