Salient features of USM3D-ME
- Full Navier-Stokes: includes all cross terms
- Thermodynamic models
- perfect gas for AIR
- Parallel processing
- Parallel execution on multiple CPUs using decomposed zonal grid
- Message passing through MPI
- Time integrations
- Steady State (Implicit Point Gauss-Seidel & Explicit Runge-Kutta)
- 2nd Order Time Stepping
- Upwind flux functions
- Roe’s Flux Difference Splitting (FDS)
- Van Leer’s Flux Vector Splitting (FVS)
- HLLE scheme
- HLLC scheme
- Flux Limiters
- Barth Jesperson
- Van Leer
- Van Albada
- Venkat
- Minmod
- Turbulence Models
- Spalart-Allmaras (SA) turbulence model
- Standard SA model
- SA model with negative provisions (SA-neg)
- Rotation correction
- Quadratic Constitutive Relation (QCR-2000) for calculating Reynolds stresses
- Transition tripping at prescribed locations
- Spalart-Allmaras (SA) turbulence model
- Boundary conditions
- Freestream inflow
- Symmetry
- Supersonic outflow
- Characteristic inflow/outflow
- Solid no-slip wall
- Solid turbulent wall function
- Solid tangency wall
- Trailing-edge wake simulation
- Propulsion systems
- coupled jet exhaust with inlet
- source-term based propeller model
- Portable (Linux clusters, SGI, HP, IBM, Mac)
- x – longitudinal body axis (positive in downstream direction)
- y – spanwise or lateral body axis (positive to pilot’s right if computing
lateral/directional coefficients on full configuration. Otherwise the y-direction is not important.) - z – vertical direction in body axis (positive upward)
- Alpha (x-z plane) – Positive nose up
- Beta (y-z plane) – Positive for yaw to the left
- Pitching moment (x-z plane) – Positive pitch up
- Rolling moment (y-z plane) – Positive roll right
- Yawing moment (x-y plane) – Positive yaw right
Convention used for coordinate system in USM3D-ME
It is important to construct the computational grid in the correct coordinate system in order for alpha, beta, and the force & moments to be interpreted correctly.
The required coordinate system is:
Force & Moment sign conventions:
Nondimensionalization used in USM3D-ME
The flow solver employs following scheme for the nondimensionalization of various parameters of interest.
Considering the convention used for the coordinate system in USM3D-ME and the nondimensionalization scheme described above, the freestream and other relevant quantities assume the following nondimensional values/form.
where:
Sutherland’s law for the molecular viscosity mentioned above is given by: