Abstract

This work examined transient flows that occur in shock tunnels. Two areas were examined. The first area was the end wall region of the driven tube. This region forms the reservoir for the nozzle section. The second area was the transient flow in the nozzle itself. These transient flows are important when determining test times and test conditions. It is very difficult to study these transient flows experimentally; therefore, computational fluid dynamics (CFD) was used.

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