Wissenschaftlicher Mitarbeiter


Foto von Christian Schäffer

Christian Schäffer, M.Sc.

Technische Universität München

Lehrstuhl für Turbomaschinen und Flugantriebe (Prof. Gümmer)

Postadresse

Postal:
Boltzmannstr. 15
85748 Garching b. München

Forschungsschwerpunkte

  • Experimentelle Untersuchungen am Axialverdichterprüfstand (HSRC)
  • Durchführung des experimentellen Teils im Projekt FloCoTec
  • Schwerpunkt: Instationäre Strömungsmesstechnik (FRAP, Hitzdrahtanemometrie, Entropiesonde)

Aufgaben in Lehre und Administration

  • Tech-Lead
  • IT-Systemadministrator

Veröffentlichungen

2022

  • Schäffer, Christian; Speck, Konstantin; Gümmer, Volker: Numerical Calibration and Investigation of the Influence of Reynolds Number on Measurements With Five-Hole Probes in Compressible Flows. Journal of Turbomachinery 144 (9), 2022 mehr…
  • Speck, Konstantin; Schäffer, Christian; Gümmer, Volker: Design of a Small Pressure Chamber to Evaluate Probe Calibrations at Varying Reynolds Numbers. XXVI Biennial Symposium on Measuring Techniques in Turbomachinery, 2022 mehr…

2021

  • Schäffer, Christian; Speck, Konstantin; Gümmer, Volker: Numerical Calibration and Investigation of the Influence of Reynolds Number on Measurements With Five-Hole Probes in Compressible Flows. ASME Turbo Expo, 2021 mehr…

2018

  • Fuchs, F.; Schäffer, C.; Gümmer, V.: Experimental Investigation of a Radial Turboshaft Engine intake. 54nd AIAA/SAE/ASEE Joint Propulsion Conference, 2018 mehr…

2017

  • Kerler, M.; Schäffer, C.; Erhard, W.; Gümmer, V.: Experimental Investigation of an Engine Quick-Start System with Compact Air Supply for Rotorcraft Application. 17th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2017 mehr…
  • Kerler, M.; Schäffer, C.; W. Erhard, V. Gümmer: Operational Aspects of an Engine Quick-Start System with Compact Air Supply for Rotorcraft Application. Deutscher Luft- und Raumfahrtkongress, 2017 mehr…

2016

  • Kerler, M.; Schäffer, C.; Erhard, W.; Gümmer, V.: Design of an Airworthy Turboshaft Engine Quick-Start System with Compact Pressurized Air Supply for Rotorcraft Application. 42nd European Rotorcraft Forum, 2016 mehr…
  • Kerler, M.; Schäffer, C.; Erhard, W.; Gümmer, V.: Design Parameter Identification of the Air Supply for a Turboshaft Engine Quick-Start System. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016AIAA-2016-5062 mehr…

2015

  • Kerler, M.; Schäffer, C.; Erhard, W.: Design of an Engine Quickstart System for Rotorcraft Application. 11th European Turbomachinery Conference, 2015 mehr…