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2019

Rähse, T. S., Stathopoulos, P., Schäpel, J.-S., Arnold, F. and King, R. (2019). On the Influence of Fuel Stratification and Its Control on the Efficiency of the Shockless Explosion Combustion Cycle. Journal of Engineering for Gas Turbines and Power, 011024.


2018

Schäpel, J.-S., King, R., Yücel, F., Völzke, F., Paschereit, C. O. and Klein, R. (2018). Fuel Injection Control for a Valve Array in a Shockless Explosion Combustor. ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, V006T05A007.


2017

Reichel, T. G., Schäpel, J.-S., Bobusch, B. C., Klein, R., King, R. and Oliver Paschereit, C. (2017). Shockless Explosion Combustion: Experimental Investigation of a New Approximate Constant Volume Combustion Process. Journal of Engineering for Gas Turbines and Power


Schäpel, J.-S., Wolff, S., Schulze, P., Berndt, P., Klein, R., Mehrmann, V. and King, R. (2017). State estimation for reactive Euler equation by Kalman Filtering. CEAS Aeronautical Journal


2016

Schäpel, J.-S., Reichel, T., Klein, R., Paschereit, C. and King, R. (2016). Online Optimization Applied to a Shockless Explosion Combustor. Processes, 48.


2015

Wolff, S., Schäpel, J.-S., Berndt, P. and King, R. (2015). State Estimation for the Homogeneous 1-D Euler Equation by Unscented Kalman Filtering. Proceedings of the ASME Dynamic Systems and Control Conference


Schäpel, J.-S., King, R., Bobusch, B., Moeck, J. and Paschereit, C. O. (2015). Adaptive Control of Mixture Profiles for a Combustion Tube. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition


Publikationsliste

2020

Berthold, A., Haucke, F. and Weiss, J. (2020). Flow Field Analysis of a Dynamically Forced Impingement Jet Array. AIAA SciTech Forum


Werder, T., Liebich, R., Neuhäuser, K., Behnsen, C. and King, R. (2020). Active Flow Control Utilizing an Adaptive Blade Geometry and an Extremum Seeking Algorithm at Periodically Transient Boundary Conditions. Proceedings of ASME Turbo Expo 2020,, GT2020-15591.


2019

Zander, L., Tornow, G., Klein, R. and Djordjevic, N. (2019). Knock Control in Shockless Explosion Combustion by Extension of Excitation Time. Active Flow and Combustion Control 2018, 151–166.


Herbig, M., Heinrich, A. and Peitsch, D. (2019). Design of a Testrig to evaluate Axial Turbine Performance underpulsating and steady Inflow Conditions. Deutscher Luft- und Raumfahrtkongress, Nr. DGLR-2019-490177, Darmstadt


Heinrich, A., Herbig, M., Peitsch, D., Topalovic, D. and King, R. (2019). A Testrig to evaluate Turbine Performanceand Operational Strategies under pulsating Inflow Conditions. AIAA Propulsion and Energy 2019 Forum, Nr. AIAA 2019-4039. American Institute of Aeronautics and Astronautics


Heinrich, A., Berthold, A., Topalovic, D., King, R., Haucke, F. and Peitsch:, D. (2019). Turbine Design Challengesinduced by Pressure Gain Combustion. Deutscher Luft- und Raumfahrtkongress, Nr. DGLR-2019-490177


Rezay Haghdoost, M., Edgington-Mitchell, D. M., Paschereit, C. O. and Oberleithner, K. (2019). Investigation of the Exhaust Flow of a Pulse Detonation Combustor at different Operating Conditions based on High-Speed Schlieren and PIV. AIAA Scitech 2019 Forum, 1512., 29.


Schulze, P., Reiss, J. and Mehrmann, V. (2019). Model Reduction for a Pulsed Detonation Combuster via Shifted Proper Orthogonal Decomposition. Active Flow and Combustion Control 2018


Sroka, M., Engels, T., Krah, P., Mutzel, S., Schneider, K. and Reiss, J. (2019). An Open and Parallel Multiresolution Framework Using Block-Based Adaptive Grids. Active Flow and Combustion Control 2018, 305–319.


Staats, M., Ebert, C. and Weiss, J. (2019). Experimental Investigations on Active Flow Control Applied to anAsymmetric Compressor Cascade. AIAA Aviation Forum 2019, ARC - Aerospace Research Central,2019. American Institute of Aeronautics and Astronautics.


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