USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynolds stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model.Wang, Qun-Zhen and Massey, Steven J. and Abdol-Hamid, Khaled S.Langley Research CenterAPPLICATIONS PROGRAMS (COMPUTERS); NAVIER-STOKES EQUATION; UNSTRUCTURED GRIDS (MATHEMATICS); TURBULENCE MODELS; AIRFOILS; WINGS; VISCOUS FLOW; FLAT PLATES; INVISCID FLOW; COMPUTERIZED SIMULATION; COMPUTATIONAL FLUID DYNAMICS; K-EPSILON TURBULENCE MODEL; REYNOLDS STRESS; STRESS ANALYSIS; FLOW DISTRIBUTION; FINITE VOLUME METHOD; VORTICES; EDDY VISCOSITY