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Majid Asli
Majid Asli
Brandenburg University of Technology
Verified email at b-tu.de - Homepage
Title
Cited by
Cited by
Year
Numerical analysis of wind turbine airfoil aerodynamic performance with leading edge bump
M Asli, B Mashhadi Gholamali, AM Tousi
Mathematical Problems in Engineering 2015, 2015
362015
Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
M Asli, P Stathopoulos, CO Paschereit
Journal of Engineering for Gas Turbines and Power 143 (6), 061011, 2021
232021
A fast approach for unsteady compressor performance simulation under boundary condition caused by pressure gain combustion
N Neumann, M Asli, N Garan, D Peitsch, P Stathopoulos
Applied Thermal Engineering 196, 117223, 2021
92021
Performance analysis of axial flow compressor and part load consideration in a gas turbine application
M Asli, AM Tousi
Journal of Thermal Science and Technology 8 (3), 476-487, 2013
92013
A robust one-dimensional approach for the performance evaluation of turbines driven by pulsed detonation combustion
M Asli, N Garan, N Neumann, P Stathopoulos
Energy Conversion and Management 248, 114784, 2021
82021
2D Euler modeling of rotating detonation combustion in preparation for turbomachinery matching
R Klopsch, N Garan, M Bohon, E Bach, M Asli, P Stathopoulos
AIAA SciTech 2022 Forum, 0836, 2022
72022
Numerical Investigation of a Turbine Guide Vane Exposed to Rotating Detonation Exhaust Flow
M Asli, C Cuciumita, P Stathopoulos, CO Paschereit
ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, 2019
72019
Thermal management challenges in hybrid-electric propulsion aircraft
M Asli, P König, D Sharma, E Pontika, J Huete, KR Konda, ...
Progress in Aerospace Sciences 144, 2024
22024
Investigation of stationary vanes aerodynamic performance under different rdc exhaust
M Asli, P Stathopoulos, CO Paschereit
The University of Queensland, 2020
22020
On the Potentials of the Integration of Pressure Gain Combustion with a Hybrid Electric Propulsion System
D Kim, M Asli, K Höschler
Aerospace 10 (8), 710, 2023
12023
An Optimization Methodology for Turbines Driven by Pulsed Detonation Combustors
M Asli, P Stathopoulos
Journal of Engineering for Gas Turbines and Power 144 (11), 111004, 2022
12022
Effect of Blade Setting Angle on Damping Role of Turbine Guide Vanes Downstream of an RDC
M Asli, P Stathopoulos, CO Paschereit
Proceedings of the International Gas Turbine Congress 2019 Tokyo, 2019
12019
Performance prediction of axial flow turbomachines using a modified one dimensional method
M Asli, AM Tousi
International Journal of Scientific & Engineering Research 4 (7), 1486-1491, 2013
12013
Sensitivity Analysis of a Centrifugal Compressor Using the Linearization Method
M Asli, AM Tousi
Fluids Engineering Division Summer Meeting 44403, 1785-1790, 2011
12011
Film Cooling Modeling in a Turbine Working under the Unsteady Exhaust Flow of Pulsed Detonation Combustion
GR Varatharajulu Purgunan, M Asli, T Nacci, DA Misul, S Salvadori, ...
Energies 17 (6), 1312, 2024
2024
Film Cooling Modeling in a Turbine Working under the Unsteady Exhaust Flow of Pulsed Detonation Combustion
GRV Purgunan, M Asli, T Nacci, DA Misul, S Salvadori, P Stathopoulos
Energies 17 (6), 1-20, 2024
2024
Investigation on the effects of blade leading-edge protuberances on the aerodynamic performance of an axial transonic compressor
M Asli, S Patkar, K Höschler
15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics, 2023
2023
On the potentials of the integration of pressure gain combustion with a hybrid electric propulsion system
M Asli, D Kim, K Höschler
2023
On the Potentials of the Integration of Pressure Gain Combustion with a Hybrid Electric Propulsion System. Aerospace 2023, 10, 710
D Kim, M Asli, K Höschler
2023
Turbine design development for pressure gain combustion engines
M Asli
Technical University of Berlin, 2022
2022
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