Theo dõi
Mohammad Rezay Haghdoost
Mohammad Rezay Haghdoost
Email được xác minh tại tu-berlin.de - Trang chủ
Tiêu đề
Trích dẫn bởi
Trích dẫn bởi
Năm
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
272020
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
252022
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
152021
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
132019
Uncertainty Quantification of Kiel Probes for RDC Applications
E Bach, BS Thethy, DM Edgington-Mitchell, M Rezay Haghdoost, ...
AIAA Scitech 2021 Forum, 0293, 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
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
112018
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
92019
Numerical and experimental evaluation of shock dividers
M Rezay Haghdoost, BS Thethy, M Nadolski, B Seo, CO Paschereit, ...
Shock Waves, 1-17, 2022
82022
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
82019
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
72021
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
62022
Redistribution of transient shock waves using shock dividers
BS Thethy, M Rezay Haghdoost, CO Paschereit, D Honnery, ...
AIAA Scitech 2020 Forum, 0925, 2020
42020
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
32020
Pulse detonation exhaust and methods for damping its transient characteristic
MR Haghdoost
Technische Universität Berlin, 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
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
Fabian Habicht1 (✉), Fatma Cansu Yücel¹, Myles Bohon²
MR Haghdoost, K Oberleithner
Active Flow and Combustion Control 2021: Papers Contributed to the …, 2021
2021
Pressure fluctuations in air supply of a valveless PDC-multitube
FE Habicht, FC Yücel, MR Haghdoost, K Oberleithner, CO Paschereit
ICPCD 2020, 2020
2020
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