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Interactive grid generation for turbomachinery flow field simulations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reno Sr., Charles Choo, Yung K. Eiseman, Peter R. |
| Copyright Year | 1988 |
| Description | The control point form of algebraic grid generation presented provides the means that are needed to generate well structured grids for turbomachinery flow simulations. It uses a sparse collection of control points distributed over the flow domain. The shape and position of coordinate curves can be adjusted from these control points while the grid conforms precisely to all boundaries. An interactive program called TURBO, which uses the control point form, is being developed. Basic features of the code are discussed and sample grids are presented. A finite volume LU implicit scheme is used to simulate flow in a turbine cascade on the grid generated by the program. |
| File Size | 3422218 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890002346 |
| Archival Resource Key | ark:/13960/t9p31s78d |
| Language | English |
| Publisher Date | 1988-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Cascade Flow Structured Grids Mathematics Computer Graphics Flow Distribution Coordinates Finite Volume Method Turbomachinery Computerized Simulation Computational Grids Grid Generation Mathematics Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
