Euler solutions for an unbladed jet engine configurationAn Euler solution for an axisymmetric jet engine configuration without blade effects is presented. The Euler equations are solved on a multiblock grid which covers a domain including the inlet, bybass duct, core passage, nozzle, and the far field surrounding the engine. The simulation is verified by considering five theoretical properties of the solution. The solution demonstrates both multiblock grid generation techniques and a foundation for a full jet engine throughflow calculation.
Document ID
19920045577
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stewart, Mark E. M. (NASA Lewis Research Center Cleveland, OH, United States)