Supersonic combustion / Spray combustion / Turbulent combustion / Scramjet modeling
-
Northwestern Polytechnical University
- Xi'an, Shaanxi, China
-
18:05
(UTC -12:00)
-
Total Temperature and Total Pressure Calculations for Compressible Flow in OpenFOAM-v2212
C UpdatedJul 28, 2025 -
iKOmegaSST Public
Improved SST turbulence model for supersonic flows with adverse pressure gradients (APG)/separation
-
-
ymcConeInjection Public
Fixed the bug where particles can not enter after restarting the computation using the ConeInjection model in OpenFOAM.com
C UpdatedJan 12, 2024