Solver for low Mach no. flows with adiabatic thermodynamics and updated pressure-velocity coupling given by the RCM interpolation procedure described in
Knacke, T. (2013). Potential effects of Rhie & Chow type interpolations in airframe noise simulations. In: Schram, C., Dénos, R., Lecomte E. (ed): Accurate and efficient aeroacoustic prediction approaches for airframe noise, VKI LS 2013-03.
Original code supplied by Thilo Knacke, CFD Software E+F GmbH contact: email@example.com
Integrated into OpenFOAM by OpenCFD Ltd.