The infrastructure at the Institute of Jet Propulsion offers unique test facilities and capabilities for both experimental and numerical research activities:
- High Speed Cascade Wind Tunnel (HGK)
- Instationary Flow Generator (EIZ)
- Multi-Purpose Wind Tunnel (MZW)
-
Variable Inlet Guide Vane Test Facility (ELA-P)
Aero Engine Test Facility (TVA)
- Full Scale Engine Test Bed
- Scaled Propulsion System Test Bed
- Scaled Engine Altitude Test Facility (under construction)
- Up-to-date computational infrastructure
- Competences with different flow solvers
- DLR TRACE
- ANSYS CFX / Fluent