Transient blade row simulations in turbomachinery are needed either to improve the aerodynamic performance predictions or because the flow interaction we are trying to resolve and predict is unsteady in nature such as aeromechanical, aerothermodynamic or aeroacoustic interactions. Because the blade pitch is not similar between the rows of turbine or compressor, a transient blade row simulation will usually require the modeling of the full wheel (or full geometry). This constraint renders these simulations not practical and in many cases prohibitive as analysis or design tools. Continue reading
As you have probably heard, in January of this year, ANSYS 16.0 was released with a full set of new features and exciting enhancements covering our entire simulation portfolio (see more here). But in this blog, I would like to tell you a little more about turbomachinery blade row flow modeling capability in ANSYS 16.0.
Transient blade row (TBR) simulation is an important analysis and design tool, enabling turbomachinery designers to reliably improve the performance and predict the durability of rotating machinery. Traditional transient simulation methods are expensive since it requires simulation of all blades in the full 360 degrees to accurately account for the pitch difference between adjacent blade rows. However, ANSYS CFX pitch-change methods resolve this challenge by providing time accurate unsteady turbomachinery flow simulations on just a small sector of the machine annulus (typically simulating only one or a few blades, a reduced blade row model), thus tremendously reducing computing cost resources and and reducing the overall time to obtain the simulation. Continue reading
At ANSYS, we are continually improving our turbomachinery simulation capabilities. Some recent improvements are proving useful to engine manufacturers, enabling them to better understand the on-wing performance of their new fuel-efficient engines.
Fans in modern aircraft engines are very important in that they provide most of the thrust required by the aircraft. Their environment is very challenging though as they are frequently subjected to non-uniform inflow conditions. These conditions could be either due to flight operating requirements such as take-off and landing, the engine nacelle installation configuration, wake interference from aircraft fuselage or cross-flow wind conditions. Similarly, industrial land-based gas turbines in power plants can be subjected to inlet flow distortion due to upstream ducting or installation maintenance deterioration. Continue reading