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Method and apparatus for automatically generating airfoil performance tables
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2006 |
| Description | One embodiment of the present invention provides a system that facilitates automatically generating a performance table for an object, wherein the object is subject to fluid flow. The system operates by first receiving a description of the object and testing parameters for the object. The system executes a flow solver using the testing parameters and the description of the object to produce an output. Next, the system determines if the output of the flow solver indicates negative density or pressure. If not, the system analyzes the output to determine if the output is converging. If converging, the system writes the output to the performance table for the object. |
| File Size | 1293615 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080008642 |
| Archival Resource Key | ark:/13960/t5v74df4k |
| Language | English |
| Publisher Date | 2006-10-17 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Airfoils Patents Fluid Flow Inventions Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |
