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Transonic wing shape optimization using a genetic algorithm
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pulliam, Thomas H. Holst, Terry L. |
| Copyright Year | 2002 |
| Description | A method for aerodynamic shape optimization based on a genetic algorithm approach is demonstrated. The algorithm is coupled with a transonic full potential flow solver and is used to optimize the flow about transonic wings including multi-objective solutions that lead to the generation of pareto fronts. The results indicate that the genetic algorithm is easy to implement, flexible in application and extremely reliable. |
| File Size | 444666 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020073158 |
| Archival Resource Key | ark:/13960/t6d26w60k |
| Language | English |
| Publisher Date | 2002-07-05 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Transonic Flow Wings Aerodynamic Configurations Shape Optimization Wing Profiles Design Analysis Genetic Algorithms Potential Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
