This report outlines the development of a general purpose aerodynamic solver for compressible turbulent flows. Turbulent closure is achieved using either two-equation or Reynolds stress transport equations. The applicable equation set consists of Favreaveraged conservation equations for the mass, momentum and total energy, and transport equations for the turbulent stresses and turbulent dissipation rate. In order to develop a scheme with good shock-capturing capabilities, good accuracy and… CONTINUE READING