Experimental Characterization of Axisymmetric Base Flows with Propulsive Jet (B04)

The project provides experimental simulation of supersonic afterbody flows with high-speed propulsive jets. This allows characterizing the aerodynamic interactions of dual-bell nozzles with the external flow around an axisymmetric afterbody. Time-resolving pressure measurements will be used to describe aerodynamic loads, while the results of hot-wire anemometry and PIV will characterize velocity fluctuations and turbulent transport. The robustness of passive flow control means is assessed by varying Mach number, angle of attack and nozzle flow parameters.

DFG Programme CRC/Transregios

Subproject of TRR 40:  Technological Foundations for the Design of Thermally and Mechanically Highly Loaded Components of Future Space Transportation Systems

Applicant Institution Technische Universität München (TUM)

Co-Applicant Institution Technische Universität Braunschweig

Project Heads Professor Dr.-Ing. Rolf Radespiel; Dr.-Ing. Peter Scholz