Table 5: Critical value of $\alpha $ for damping of the fundamental mode as a function of the Mach number and $\chi $, the ratio of the temperature of the CDL to the pre-shock temperature. This table is an extension of Table 3 where $\alpha _{\rm cr}$ is listed for $\chi =1$.
M $\chi $
  1.0 0.5 0.1 0.01
1.40 -1.8 -0.6 -0.2 -0.1
2.00 -1.2 -0.6 -0.2 -0.1
3.00 -0.7 -0.5 -0.2 -0.1
5.00 -0.4 -0.3 -0.1 -0.1
10.0 -0.1 -0.1 0.1 0.3
20.0 0.2 0.2 0.2 0.3
40.0 0.3 0.3 0.3 0.3
100 0.4 0.4 0.4 0.4


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