Aircraft Flow Analysis

$markdown-enabled$ Calculates the pressure, velocity, and surface forces on an implicit body. The implicit body must be oriented in the default aircraft position with flow direction aligned to the positive X-axis, Y-axis the starboard/right wing direction and Z-axis pointing upward (lift direction). The solution uses a Lattice Boltzmann Method. A transient simulation is initiated and continues until the flow reaches a statistically steady state, then returns time-averaged pressure, velocity fields, along with the force on the implicit body surfaces. Streamlines will be calculated on the time-averaged velocity results. This block requires an NVIDIA GPU.