Segui
Zhe Liu
Zhe Liu
Virtual Propulsion Engineer at General Motors
Email verificata su umich.edu - Home page
Titolo
Citata da
Citata da
Anno
Characterization of a supersonic turbine downstream of a rotating detonation combustor
Z Liu, J Braun, G Paniagua
Journal of Engineering for Gas Turbines and Power 141 (3), 031501, 2019
732019
Performance of axial turbines exposed to large fluctuations
Z Liu, J Braun, G Paniagua
53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4817, 2017
332017
Thermal power plant upgrade via a rotating detonation combustor and retrofitted turbine with optimized endwalls
Z Liu, J Braun, G Paniagua
International Journal of Mechanical Sciences 188, 105918, 2020
292020
Characterization of a supersonic turbine downstream of a rotating detonation combustor
Z Liu, J Braun, G Paniagua
Turbo Expo: Power for Land, Sea, and Air 51043, V003T06A021, 2018
202018
Characterization of an integrated nozzle and supersonic axial turbine with a rotating detonation combustor
J Braun, DG Cuadrado, V Andreoli, G Paniagua, Z Liu, J Saavedra, ...
AIAA Propulsion and Energy 2019 Forum, 3873, 2019
182019
Design of directional probes for high-frequency turbine measurements
Z Liu, G Paniagua
Journal of Engineering for Gas Turbines and Power 140 (1), 011601, 2018
172018
Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser
Z Liu, J Braun, G Paniagua
International Journal of Turbo & Jet-Engines 40 (1), 1-10, 2023
152023
Three dimensional optimization for subsonic axial turbines operating at high unsteady inlet Mach number
Z Liu, J Braun, G Paniagua
2018 Joint Propulsion Conference, 4480, 2018
112018
Performance Analysis and Modeling of the Two-Stage Wave Disk Engine
Z Liu, P Akbari
1st Thermal and Fluids Engineering Summer Conference, 2015
32015
Unsteady Heat Transfer Assessment of Supersonic Turbines Downstream of a Rotating Detonation Combustor
Z Liu, LB Inhestern, J Braun, G Paniagua
ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, 2019
22019
Numerical analysis on the effect of CTAP measurements in pulse and rotating detonation combustors
Z Liu, J Braun, J Saavedra, G Paniagua
AIAA Propulsion and Energy 2019 Forum, 4378, 2019
12019
Directional probe for high temperature flows
GP Perez, DG Cuadrado, V Andreoli, J Braun, Z Liu
US Patent 11,530,937, 2022
2022
Characterization of Axial Turbines for Pressure Gain Combustion
Z Liu
Purdue University, 2019
2019
Developments in High Frequency Directional Probes for High Temperature Applications
L Bhatnagar, J Braun, V Andreoli, DG Cuadrado, Z Liu, G Paniagua
Proceedings of the XXIV Biennial Symposium on Measuring Techniques in …, 2018
2018
On the ability of conventional aerodynamic probes to resolve high frequency phenomena
Z Liu, G Paniagua
Proceedings of the XXIII Biennial Symposium on Measuring Techniques in …, 2016
2016
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
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