Loading...
Please wait, while we are loading the content...
Similar Documents
Robust, optimal subsonic airfoil shapes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 2008 |
| Description | Method system, and product from application of the method, for design of a subsonic airfoil shape, beginning with an arbitrary initial airfoil shape and incorporating one or more constraints on the airfoil geometric parameters and flow characteristics. The resulting design is robust against variations in airfoil dimensions and local airfoil shape introduced in the airfoil manufacturing process. A perturbation procedure provides a class of airfoil shapes, beginning with an initial airfoil shape. |
| File Size | 1477486 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20090002564 |
| Archival Resource Key | ark:/13960/t5cc6038v |
| Language | English |
| Publisher Date | 2008-11-18 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Patents Inventions Flow Characteristics Airfoils Shapes Perturbation Manufacturing Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |