CHT V2.0 Analysis on the Ramjet Fuel Injectors Manifold

About this project

Conjugate Heat transfer Analysis on the manifold located upstream of the ramjet fuel injector is performed using SimScale CHT V2.0 Solver. The flow field of the hot fuel JP-7 flowing through the manifold is simulated and the wall temperature of the manifold is computed. This experiment essentially duplicates the conditions of a regeneratively fuel cooled hypersonic ramjet engine flow path of heat sink construction to simulate the actual conditions the engine would be operated at by using a facility fuel heater. In order to match these conditions correctly, a detailed thermal analysis on upstream fuel delivery components(manifold) is required.