Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery · 1990 · 19 citations · 0 references
EngineeringAerospace SimulationFluid MechanicsSimulationGas DynamicNumerical SimulationIn-cylinder FlowModeling And SimulationRamscram CodeRocket EngineComputer EngineeringComputational Fluid DynamicsPropulsionMultiphase FlowSupersonic CombustionAerospace EngineeringEquilibrium ThermodynamicsAerodynamicsRocket EnginesAerospace Propulsion
With the resurgence of interest in high supersonic and hypersonic flight there is a need to simulate airbreathing engines which may be used in this flight regime. To meet this requirement the RAMSCRAM code was developed. The code calculates one-dimensional flow properties at each component interface and the overall performance of the engine. It uses equilibrium thermodynamics which accounts for dissociation and allows for any fuel or combination of fuels. The program can simulate ramjet, scramjet, rocket, and ducted rocket engines.