Dynamic evolution of a transient supersonic trailing jet induced by a strong incident shock wave M Rezay Haghdoost, D Edgington-Mitchell, M Nadolski, R Klein, ... Physical Review Fluids 5 (7), 073401, 2020 | 24 | 2020 |
Kiel probes for stagnation pressure measurement in rotating detonation combustors E Bach, BS Thethy, D Edgington-Mitchell, M Rezay Haghdoost, ... AIAA Journal 60 (6), 3724-3735, 2022 | 19 | 2022 |
Investigation of the exhaust flow of a pulse detonation combustor at different operating conditions based on high-speed schlieren and PIV M Rezay Haghdoost, DM Edgington-Mitchell, CO Paschereit, ... AIAA Scitech 2019 Forum, 1512, 2019 | 14 | 2019 |
High-speed schlieren and particle image velocimetry of the exhaust flow of a pulse detonation combustor MR Haghdoost, D Edgington-Mitchell, CO Paschereit, K Oberleithner AIAA Journal 58 (8), 3527-3543, 2020 | 12 | 2020 |
Mitigation of pressure fluctuations from an array of pulse detonation combustors MR Haghdoost, BS Thethy, D Edgington-Mitchell, F Habicht, J Vinkeloe, ... Journal of Engineering for Gas Turbines and Power 143 (7), 071011, 2021 | 11 | 2021 |
Uncertainty Quantification of Kiel Probes for RDC Applications E Bach, BS Thethy, DM Edgington-Mitchell, M Rezay Haghdoost, ... AIAA Scitech 2021 Forum, 0293, 2021 | 10 | 2021 |
Influence of nozzle geometry on detonation-driven and shock-driven transient supersonic jet flow B Thethy, M Rezay Haghdoost, K Oberleithner, D Honnery, ... 24th International Society for Air Breathing Engines Conference, 1-22, 2019 | 10 | 2019 |
Experimental Investigation of Solid Tracer Particle Response Across a Mach Disk by PIV and Schlieren MR Haghdoost, J Förster, D Edgington-Mitchell, K Oberleithner 19th International Symposium on Applications of Laser and Imaging Techniques …, 2018 | 10 | 2018 |
Validation of under-resolved numerical simulations of the PDC exhaust flow based on high speed schlieren M Nadolski, MR Haghdoost, JAT Gray, D Edgington-Mitchell, ... Active Flow and Combustion Control 2018: Papers Contributed to the …, 2019 | 8 | 2019 |
Numerical and experimental evaluation of shock dividers M Rezay Haghdoost, BS Thethy, M Nadolski, B Seo, CO Paschereit, ... Shock Waves, 1-17, 2022 | 6 | 2022 |
Acoustic modes in a plenum downstream of a multitube pulse detonation combustor F Habicht, FC Yücel, M Rezay Haghdoost, K Oberleithner, CO Paschereit AIAA Journal 59 (11), 4569-4580, 2021 | 5 | 2021 |
Diffraction of shock waves through a non-quiescent medium BS Thethy, MR Haghdoost, R Kirby, B Seo, M Nadolski, C Zenker, ... Journal of Fluid Mechanics 944, A39, 2022 | 3 | 2022 |
Redistribution of transient shock waves using shock dividers BS Thethy, M Rezay Haghdoost, CO Paschereit, D Honnery, ... AIAA Scitech 2020 Forum, 0925, 2020 | 3 | 2020 |
Evaluation of shock dividers using numerical and experimental methods M Rezay Haghdoost, BS Thethy, M Nadolski, R Klein, D Honnery, ... AIAA Scitech 2020 Forum, 0926, 2020 | 3 | 2020 |
Pressure Fluctuations in an Annular Plenum Downstream of a Multi-tube Pulse Detonation Combustor F Habicht, FC Yücel, M Bohon, MR Haghdoost, K Oberleithner, ... Active Flow and Combustion Control 2021: Papers Contributed to the …, 2022 | 1 | 2022 |
Pulse detonation exhaust and methods for damping its transient characteristic M Rezay Haghdoost | | 2022 |
Pulse Detonation Exhaust and Methods for Damping Its Transient Characteristic MR Haghdoost Technische Universität Berlin, 2022 | | 2022 |
Computational Simulation of an Exhaust Plenum Charged by a Multi-tube Pulsed Detonation Combustor M Nadolski, MR Haghdoost, K Oberleithner, R Klein Active Flow and Combustion Control 2021: Papers Contributed to the …, 2022 | | 2022 |
Pressure fluctuations in air supply of a valveless PDC-multitube FE Habicht, FC Yücel, MR Haghdoost, K Oberleithner, CO Paschereit ICPCD 2020, 2020 | | 2020 |
Auslegung und Aufbau eines skalierten Modellwindkanals zur Untersuchung von strömungsbeeinflussenden Maßnahmen in der Vorkammer des DLR-Verdichter-Prüfstands M2VP MR Haghdoost, R Meyer Technische Universität Berlin, 2015 | | 2015 |