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Mohammad Rezay Haghdoost
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Dynamic evolution of a transient supersonic trailing jet induced by a strong incident shock wave
MR Haghdoost, D Edgington-Mitchell, M Nadolski, R Klein, K Oberleithner
Physical Review Fluids 5 (7), 073401, 2020
232020
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
152022
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
142019
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
122021
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
122020
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
102019
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
102018
Uncertainty Quantification of Kiel Probes for RDC Applications
E Bach, BS Thethy, DM Edgington-Mitchell, M Rezay Haghdoost, ...
AIAA Scitech 2021 Forum, 0293, 2021
82021
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
72019
Numerical and experimental evaluation of shock dividers
M Rezay Haghdoost, BS Thethy, M Nadolski, B Seo, CO Paschereit, ...
Shock Waves, 1-17, 2022
52022
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
52021
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
42020
Redistribution of transient shock waves using shock dividers
BS Thethy, M Rezay Haghdoost, CO Paschereit, D Honnery, ...
AIAA Scitech 2020 Forum, 0925, 2020
32020
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
12022
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
12022
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
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