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Taha Rezzag
Taha Rezzag
在 ucf.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
The effect of premixed stratification on the wave dynamics of a rotating detonation combustor
R Burke, T Rezzag, I Dunn, W Flores, K Ahmed
International Journal of Hydrogen Energy 46 (54), 27816-27826, 2021
332021
Experimental validation of rotating detonation for rocket propulsion
JW Bennewitz, JR Burr, BR Bigler, RF Burke, A Lemcherfi, T Mundt, ...
Scientific Reports 13 (1), 14204, 2023
102023
A Kinematic Study of Individual Rotating Detonation Engine Waves Using K-Means Algorithm
T Rezzag, R Burke, K Ahmed
Turbo Expo: Power for Land, Sea, and Air 84942, V03AT04A019, 2021
72021
Characterization of injection mixing in the rotating detonation rocket engine
AM Burden, RF Burke, T Rezzag, JO Jacobson, S Schuetz, KA Ahmed
AIAA SCITECH 2023 Forum, 0572, 2023
52023
Sustainable particles seeding in air-breathing rotating detonation engine
RF Burke, T Rezzag, KA Ahmed
AIAA Scitech 2021 Forum, 0556, 2021
52021
Carbon and hydrocarbon particle seeding in air-breathing rotating detonation engine
RF Burke, T Rezzag, K Ahmed
Journal of Engineering for Gas Turbines and Power 144 (1), 011013, 2022
42022
Validation of Experimental Evidence for H2/O2 Powered Rotating Detonation Rocket Engine
RF Burke, T Rezzag, KA Ahmed
AIAA Propulsion and Energy 2021 Forum, 3672, 2021
32021
Experimental Investigation of Injector Sizing In The Rotating Detonation Rocket Engine
AM Burden, RF Burke, A Kotler, KA Ahmed, S Schuetz, T Rezzag
AIAA AVIATION 2022 Forum, 4106, 2022
22022
Development of an Automatic-Calibrating Small-Scale Thrust Stand for Rotating Detonation Rocket Engines
RF Burke, T Rezzag, A Rodriguez, K Garcia, KA Ahmed, A Kotler
AIAA SciTech 2022 Forum, 2370, 2022
22022
Dynamic Mode Decomposition Study of a RDRE Exhaust for Swirl Attenuation Using Various Nozzle Configurations
T Rezzag, RF Burke, A Rodriguez, K Garcia, B Stiehl, KA Ahmed
AIAA SciTech 2022 Forum, 0516, 2022
22022
A numerical study on the effect of hole inclination angle with imperfection on film cooling effectiveness
T Rezzag, BA Jubran
Turbo Expo: Power for Land, Sea, and Air 58646, V05AT12A007, 2019
22019
Rotating detonation engine injector and method of designing
R Burke, T Rezzag, A Kotler, K Ahmed
US Patent App. 18/111,778, 2023
12023
Development of an Automatic-Calibrating Small-Scale Thrust Stand for Rotating Detonation Rocket Engines
A Kotler, RF Burke, T Rezzag, KA Ahmed
12022
The Effect of Fuel Partial Premixing on Rotating Detonation Waves
R Burke, T Rezzag, A Kotler, K Ahmad
28th ICDERS, June, 19-24, 2022
12022
Exploration of Large Eddy Simulation with Adaptive Mesh Refinement for a High-Pressure Staged Combustion System
B Stiehl, T Genova, MK Newmyer, MK Fortin, ME Tonarely, T Rezzag, ...
AIAA SCITECH 2022 Forum, 1721, 2022
12022
On Mode Transition Phenomenon and Operating Conditions in Rotating Detonation Rocket Engines
T Rezzag-Lebza
12021
Comparison Study of Instantaneous Oscillatory Behavior Between RDREs and Air-Breathing RDEs
T Rezzag, RF Burke, KA Ahmed
AIAA Propulsion and Energy 2021 Forum, 3668, 2021
12021
Startup and Shutdown Transient Behaviors in a Rotating Detonation Engine
RF Burke, T Rezzag, KA Ahmed
AIAA SCITECH 2024 Forum, 1424, 2024
2024
Thermal Analysis of Additively Manufactured Al-F357 and Inconel 718 in High-Enthalpy Hypersonic Flows
A La Sorsa, RF Burke, T Rezzag, KA Ahmed, A Koumpias, B Friend, ...
AIAA SCITECH 2024 Forum, 2400, 2024
2024
An Investigation on the Flame Acceleration of Oxygen Enriched Ethylene Flames
R Hytovick, TR Brown, RF Burke, T Rezzag, KA Ahmed
AIAA AVIATION 2022 Forum, 4145, 2022
2022
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