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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.


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.


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


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


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



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.


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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