A wide spectrum of facilities and computational tools covers the flow range from the low-speed regime of commercial aircraft to the supersonic and hypersonic regime of atmospheric space entry. The department focuses in particular on the modeling, simulation and experimental validation of atmospheric entry flows and thermal protection systems (TPS), including transition to turbulence and stability. The experimental studies are carried out in its top level Mach 14, Mach 6 and Induction Coupled Plasma windtunnels, for which dedicated measuring techniques have been developed e.g. involving spectroscopic laser techniques. On the computational simulation side the department has developed an extendable software platform Coolfluid for high performance computational flow simulation which incorporates the research on numerical algorithms, advanced physico-chemical and plasma models as well as fluid-structure interaction and conjugate heat transfer.