Mohammad Rezay Haghdoost
Title
Cited by
Cited by
Year
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
82019
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
52019
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, 237-253, 2019
52019
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
32018
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
22020
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
12020
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
12020
Redistribution of Transient Shock Waves Using Shock Dividers
BS Thethy, M Rezay Haghdoost, CO Paschereit, D Honnery, ...
AIAA Scitech 2020 Forum, 0925, 2020
12020
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
2020
Pressure fluctuations in air supply of a valveless PDC-multitube
FE Habicht, FC Yücel, MR Haghdoost, K Oberleithner, CO Paschereit
ICPCD 2020, 2020
2020
Evaluation of Shock Dividers using Numerical and Experimental Methods
MR Haghdoost, BS Thethy, M Nadolski, R Klein, D Honnery, ...
2019
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
Mitigation of Pressure Fluctuations from an Array of Pulse Detonation Combustors
MR Haghdoost, BS Thethy, D Edgington-Mitchell, FE Habicht, J Vinkeloe, ...
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Articles 1–13