3rd most read article of 2025: Unlocking Advanced Heat Exchanger Design and Simulation with nTop Platform and ANSYS CFX

This report documents the design process of a Fuel Cooled Oil Cooler (FCOC) from initial design in CAD, process steps in nTop Platform, and final Computational Fluid Dynamics (CFD) analysis steps in ANSYS CFX.

Turquoise and silver topological illustration
Comparison of the fuel exit geometry from the gyroid core
Phot credit: nTopology

It is now possible to produce a next generation high-performance Heat Exchanger (HEX) for the aerospace industry using advanced materials and manufacturing methods.

In aviation, thrust is required to propel air and spacecraft through the atmosphere. The engine combusts fuel and extracts mechanical work from this combustion to generate the thrust required for flight. In all engines, the process of combustion and mechanical work produces excess heat that must be dissipated. Specifically, the oil in the engine needs to be cooled to maintain the lubrication of components that rotate within the engine. In modern aircraft, the fuel spends much time stored in the wings, where it gets extremely cold. As such, it can be used to cool many of the subsystems of the aircraft. A Fuel Cooled Oil Cooler (FCOC) exchanges heat between the engine oil and the fuel in such a manner that the engine oil is cooled while the fuel is heated up. This exchange of heat serves two purposes: the cooled oil properly lubricates the engine while heating the fuel prevents the formation of ice crystals within the fuel.

Learn more how a design inspired by an America Makes project leveraged additive manufacturing to increase the performance of the legacy component.