Publications - 39Publications - 39
Publications - 39Publications (39)
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JournalDrag reduction in transonic shock-wave/boundary-layer interaction using porous medium: a computational study2021 | Springer Science and Business Media Deutschland GmbH
Effectiveness of micro-vortex generators in tandem in high-speed flows2020 | American Institute of Aeronautics and Astronautics- OtherNumerical study of camber morphing in naca0012 airfoil2020 | American Institute of Aeronautics and Astronautics Inc, AIAA
- A Simplified Local Correlation-Based Zero-Equation Transition Model2020 | American Institute of Aeronautics and Astronautics
- Optimization of the Thrust to Lift Ratio using Camber Morphing in Flapping Airfoil2020 | American Institute of Aeronautics and Astronautics
OtherAdaptation of 2D unstructured mesh based on solution gradients2020 | International Centre for Numerical Methods in Engineering, CIMNE- JournalComputations of Flow past the Corrugated Airfoil of Drosophila Melanogaster at Ultra Low Reynolds Number2020 | Isfahan University of Technology
- ConferencesSecond-order interpolation techniques for accurate surface data estimation in immersed-boundary methods2018 | American Institute of Aeronautics and Astronautics Inc, AIAA
- ConferencesA convergence study of solutions using two two-equation RANS turbulence models on a finite volume solver for structured grids2018 | American Institute of Aeronautics and Astronautics Inc, AIAA
- ConferencesNumerical investigation of transonic flow over porous medium using immersed boundary method2018 | American Institute of Aeronautics and Astronautics Inc, AIAA
ArticlesAnalytical and numerical study of normal shock response in a uniform duct2018 | American Institute of Physics Inc.- ConferencesEvaluation of ramp-type micro vortex generators using swirl center tracking2018 | American Institute of Aeronautics and Astronautics Inc.
- ConferencesFlow control in Mach 4.0 inlet by slotted wedge-shaped vortex generators2017 | American Institute of Aeronautics and Astronautics Inc.
- ConferencesPassive control of normal-shock-wave/boundary-layer interaction using porous medium: Computational study2017 | American Institute of Aeronautics and Astronautics Inc, AIAA
