Research output per year
Research output per year
Project Details
Description
Within the framework of this project, the combustion chamber of a jet engine in the thrust
range of 1kN will be adapted for the combustion of hydrogen. Therefore the rotor bearings
as well as the controller of the jet engine need to be adjusted. The emissions should be
significantly improved compared to the current state of technology. The new combustion
chamber concept will be validated experimentally in a scaled version.
| Status | Finished |
|---|---|
| Effective start/end date | 1/06/13 → 31/05/16 |
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Research output
- 3 (Old data) Lecture or Presentation
-
Demonstration of an Aerodynamic Design Process for Turbomachines using Open Source Tools
Borm, O., Balassa, B., Barthmes, S., Fellerhoff, J., Kührmann, A. & Kau, H-P., 14 Jun 2010.Research output: Contribution to conference › (Old data) Lecture or Presentation
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Implementation of a Domain Scaling Approach for Turbomachinery Computations in OpenFOAM
Borm, O., Tekin, F. & Kau, H-P., 21 Jun 2010.Research output: Contribution to conference › (Old data) Lecture or Presentation
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Implementation of Rotor-Stator Interfaces in OpenFOAM
Blaim, F., Borm, O., Fröbel, T. & Kau, H-P., 10 Jul 2008.Research output: Contribution to conference › (Old data) Lecture or Presentation