Numerical results are in good agreement with some data and the method and procedure presented in this paper are verified . and then the wing ? flutter characters of a missile wing are numerical simulated with the examples of a missile wing 以某导弹翼面为算例,对弹翼的亚、跨、超音速的颤振临界速度进行了数值计算,部分计算结果与风洞计算结果相比较,一致性很好。