Development of a GPU-enabled LES Solver for Unsteady Hypersonic Flows Using Curvilinear Grids
Implementing Organization
Indian Institute of Technology Goa
Indian Institute of Technology (IIT)
About
In this project,it is proposed to develop a state-of-the-art high-fidelity implicit LES solver that can meet the requirements of low-enthalpy hypersonic simulations which is fast, scalable
and portable. The proposed code will employ a curvilinear coordinate system, which will
enable simulations over complex geometries as done for scramjet (HIFiRE and BOLT)
configurations . The validated CPU code will also be optimally ported to graphics processor units (GPUs) which can enhance its capability.
Outcome / Output
The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society.
Indian Space Research Organisation Headquarters (ISRO HQ)
Quick Information
Thrust Areas
Astronomy & Space Sciences
Focus Area
Aerospace Engineering
Status
Under Development
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