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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.

ramjet manifold | SimScale Project Library | Page 1