Toward the full CFD Simulation of expansion tubes

In order to perform ground testing in expansion tubes, it is highly desirable to characterize the facility by CFD, since the flow processing is very complex. Nevertheless 2D o 3D modelling requires tackling several questions that remains opened. The main challenge is to include piston dynamics, but for that, launcher station pressure loss must be accurately simulated. This paper explores conceptual CFD models aiming to demonstrate that these effects can be included accurately. Results show that there are significant pressure losses at the launcher brought by the supersonic flow jets found after the slots. The aim is to clear the path towards the development of a full facility model, including the long time-scale piston motion couped to the gas dynamics at the whole machine