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Analysis of inviscid and viscous flows in cascades with an explicit multiple-grid algorithm
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chima, R. V. |
| Copyright Year | 1984 |
| Description | A rapid technique is used for calculating inviscid and viscous flows in turbomachinery cascades. The Euler and thin-layer Navier-Stokes equations are solved using the original explicit MacCormack algorithm. The Baldwin-Lomax eddy viscosity model is used for turbulent flows. Convergence to a steady state is accelerated by use of a variable time-step and a multiple-grid scheme. Computer time is reduced through vectorization. Details of the numerical method are presented along with computed results for two low-speed wind tunnel turning vanes, a space shuttle fuel pump turbine rotor, and a supersonic inflow compressor rotor. The method can predict subtle viscous flow phenomena in cascades and is fast enough to be used as a design tool. |
| File Size | 912440 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840014459 |
| Archival Resource Key | ark:/13960/t70w39x71 |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aeronautics (general) Transonic Flow Vector Analysis Turbomachinery Computer Programs Navier-stokes Equation Turbomachine Blades Cascade Flow Algorithms Euler Equations of Motion Flow Distribution Wind Tunnel Tests Inviscid Flow Mathematical Models Viscous Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |