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.
Accessibility Controls
