International Journal for Numerical Methods in Fluids · 1985 · 41 citations · 9 references
EngineeringAerospace EngineeringMechanical EngineeringComputational Fluid DynamicsFinite Element AnalysisFluid DynamicsComputational AerodynamicsShock WavesTransonic AerodynamicsCompressor Blade Transonic FlowComputational Fluid Dynamics For Transonic FlowShock DynamicsTransonic FlowTransonic Flow SimulationTransonic Shock WavesTriangular ElementsVelocity Potential
Abstract Steady two‐dimensional transonic flow is calculated in cascades of compressor and turbine blades using a mesh of triangular finite elements. A velocity potential is used, the equations being solved by the Newton‐Raphson technique. The resulting computer program is fast, and is shown to give good accuracy. Shock waves are well represented, provided they are not too strong.
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Lecture Notes in Economics and Mathematical Systems
Robert J. Weiner · Journal of Policy Analysis and Management · 1985 · 1.3K citations · Full text