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High bandwidth stagnation temperature measurements in a Mach 6 gun tunnel flow

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Figure

Fig. 2. a) pitot pressure fluctuations; b) heat flux fluctuations for T0 − Tw = 10K.
Figure 1: Illustration of the apparatus and instrumentation – dimensions in mm, not to scale.
Figure 2: Stagnation pressure history measured within the barrel (5 run average).
Figure 4: Examples of probe surface temperature and heat flux data.
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