The flow-field structure and pressure gain performance of a rotating detonation engine with banded distribution of reactants have been studied using two-dimensional numerical simulations. The reactants are premixed H-2/Air mixture. An unsteady reacting flow solver named rhoHLLCFoam is developed ...
The numerical simulation is conducted through our in-house solver, BYRFoam [47], developed on the open-source computational fluid dynamics platform OpenFOAM. The RDC chamber is typically an annulus where RDWs propagate circumferentially. Show abstract Effect of obstacles on the detonation diffraction ...
The flow-field structure and pressure gain performance of the two-dimensional modeled rotating detonation combustor with discrete distribution of reactants have been studied fueled by hydrogen/air and kerosene/air. An unsteady reacting flow solver named rhoHLLCFoam is developed based on the open ...
Numerical simulation of wave mode transition in rotating detonation engine with OpenFOAM. Int. J. Hydrogen Energy 2020, 45, 19989–19995. [Google Scholar] [CrossRef] Teng, H.; Zhou, L.; Yang, P.; Jiang, Z. Numerical investigation of wavelet features in rotating detonations with a two-...
A Novel Open Source Conjugate Heat Transfer Solver for Detonation Engine Simulations. In Proceedings of the AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, Kissimmee, FL, USA, 12 January 2018. 23. Theuerkauf, S.W.; Schauer, F.; Anthony, R.; Hoke, J. Experimental Characterization of ...