..., cascade-type thrust reversers. However, any reverse thrust generation is impacted by high levels of inlet distortion generated as air is drawn into the exhaust nozzle. This paper uses both Reynolds-averaged Navier–Stokes (RANS) computations and low-speed rig experiments to explore how a representative...

... proposes an interpretation of the most striking features emerging from the experiments, with the support of numerical simulations and theoretical considerations, to shed light on the aero-thermodynamic of sCO 2 compressors. The comparisons that will be presented in this chapter are intended to show...

... purposes: base T/C and light T/C. In order to evaluate the instantaneous efficiency of each turbocharger, a combination of engine tests and a 1D simulation was conducted. In the experiments, the instantaneous exhaust gas pressures, upstream and downstream of the turbine, were measured. The instantaneous...

... have to be diverted and trapped to protect the main turbine ( 10 ). Another major concern is the safety of the reactor, as the pumps of the cooling water circuit can experience trouble with two-phase flows. Another way to purify the air coming from the sumps of aeroengines is to collect the oil...