Aerospace and defence turbomachinery systems operate under strict requirements for efficiency, compactness, reliability, weight reduction, and operational stability. Compressors, turbines, fans, and pumps must deliver the required pressure ratio, mass flow rate, flow turning, and thermal-fluid performance while operating across a wide envelope of speed, altitude, temperature, and mission conditions. The flow inside turbomachinery is highly three-dimensional and sensitive to blade loading, incidence, deviation, tip clearance, end wall losses, secondary flow, wake mixing, hub-shroud contouring, and rotor-stator interaction. Small changes in blade geometry can significantly influence pressure recovery, efficiency, stall margin, vibration risk, and thermal loading. Advanced turbomachinery design software combined with CFD validation enables early-stage performance prediction and design risk reduction.

We provide turbomachinery design, CFD analysis, and optimisation services for aerospace and defence applications. We support mean line design, 3D blade design, flow-path development, blade loading control, and performance-focused geometry generation. Designs are further validated through CFD simulations evaluating pressure ratio, mass flow rate, efficiency, tip leakage, secondary flow, flow separation, wake behaviour, and thermal-fluid performance – enabling aerospace and defence customers to develop efficient, compact, and reliable turbomachinery components for advanced propulsion, cooling, and mission-critical systems.