Equations( 8.61),(8.65), and(8.67)are important Examine them closely. Note that p2/p, p2/pi and T/T are functions of the upstream Mach number M, only P/,P/P和7/7只是上游马赫数M的函数 The upstream Mach Number M is the determining parameter for changes across a normal shock wave in a calorically pertect gas 正激波上游马赫数M1是确定量热完全气体通过正激 波特性变化的决定性参数。Equations (8.61), (8.65), and (8.67) are important. Examine them closely. Note that , and are functions of the upstream Mach number M1 only. , 和 只是上游马赫数 M1 的函数。 The upstream Mach Number M1 is the determining parameter for changes across a normal shock wave in a calorically perfect gas. 正激波上游马赫数M1是确定量热完全气体通过正激 波特性变化的决定性参数。 2 1 p2 p1 T2 T1 2 1 p2 p1 T2 T1