The previous case is a special case of the moving shock. The general case is when one gas flows into another gas with a given velocity. The only limitation is that the ``downstream' gas velocity is higher than the ``upstream'' gas velocity as shown in Figure (5.17).
The relationship between the different Mach numbers on the ``upstream'' side is
calculate the new ``improved'' Mx
| Earlier, it was shown that the shock choking phenomenon occurs when the flow is running into a still medium. This phenomenon also occurs in the case where a faster flow is running into a slower fluid. The mathematics is cumbersome but results show that the shock choking phenomenon is still there (the Mach number is limited, not the actual flow). Figure (5.16) exhibits some ``downstream'' Mach numbers for various static Mach numbers, My′, and for various static ``upstream'' Mach numbers, Mx′. The figure demonstrates that the maximum can also occurs in the vicinity of the previous value (see following question/example). |