Journal of Aircraft · 1994 · 99 citations · 15 references
Numerical AnalysisReduced Order ModelingEngineeringFluid-structure InteractionTransonic SpeedsFluid MechanicsSemi-implicit MethodNumerical SimulationMultiphysics ProblemComputer EngineeringTransport PhenomenaMultiphase FlowComputational MechanicsFluxdifference Split SchemeGrid ApproachNumerical Method For Partial Differential EquationMultiscale Modeling
A computational fluid dynamic technique is demonstrated for a time-accurate store separation event at transonic speeds. An overlapping grid approach is used coupled with an implicit Euler flow solver with a fluxdifference split scheme based on Roe's approximate Riemann solver and a six-degree-of- freedom trajectory code. All major trends of the trajectory are captured and surface pressure distributions are predicted. Three sources of error are identified and discussed.
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