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Lemke, M., Westphal, C., Reiss, J. and Sesterhenn, J. (2015). Adjoint Based Data Assimilation of Sound Sources [20]. Fortschritte der Akustik


Lemke, M. and Sesterhenn, J. (2016). Adjoint-based pressure determination from PIV data in compressible flows - Validation and assessment based on synthetic data // Adjoint-based pressure determination from PIV data in compressible flows –- Validation and assessment based on synthetic data [21]. European Journal of Mechanics - B/Fluids, 29–38.


Lemke, M., Reiss, J. and Sesterhenn, J. (2017). Adjungierten-basierte Datenassimilation zur Analyse instationärer, kompressibler und reaktiver Strömungen [22]. NAFEMS Online Magazin - Zeitschrift für numerische Simulationsmethoden und angrenzende Gebiete, p. 62 - 70.


Lang, H. M., Oberleithner, K., Paschereit, C. O. and Sieber, M. (2017). Measurement of the fluctuating temperature field in a heated swirling jet with BOS tomography [23]. Experiments in Fluids, 132:1.


Lang, H., Oberleithner, K., Paschereit, C. O. and Sieber, M. (2017). Measurement of the fluctuating temperature field in a heated swirling jet with BOS tomography [24]. Experiments in Fluids. Springer Nature, 88


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Kiesner, M. and King, R. (2017). Multivariable Closed-Loop Active Flow Control of a Compressor Stator Cascade [25]. Journal of Turbomachinery, 3371–3380.


Kiesner, M. and King, R. (2015). Closed-Loop Active Flow Control of the Wake of a Compressor Blade by Trailing-Edge Blowing [26]. ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, V02AT37A004.


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Hossbach, S., Wilke, R. and Sesterhenn, J. (2015). Identification of Material Vortices [27]. Turbulence, Heat and Mass Transfer 8


Herbig, M., Heinrich, A. and Peitsch, D. (2019). Design of a Testrig to evaluate Axial Turbine Performance underpulsating and steady Inflow Conditions [28]. 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 [29]. AIAA Propulsion and Energy 2019 Forum, Nr. AIAA 2019-4039. American Institute of Aeronautics and Astronautics


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