In this paper , some flows around naca 0012 aerofoil , m6 wing and two different blunt vehicles are simulated , the results show that the present algorithm possesses good characteristics and capability for normal mach number and for hypersonic of simple configurations 通過對naca0012翼型、 m6機(jī)翼、鈍頭以及雙鈍錐?柱體的算例驗(yàn)證,本文能很好的解決一般馬赫數(shù)問題,能夠很好的求解簡單外形的高超聲速問題,對于復(fù)雜外形飛行器還需要進(jìn)一步進(jìn)行研究驗(yàn)證。