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Computational, unsteady transonic aerodynamics and aeroelasticity about airfoils and wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Guruswamy, Guru P. Goorjian, Peter M. |
| Copyright Year | 1987 |
| Description | Research in the area of computational, unsteady transonic flows about airfoils and wings, including aeroelastic effects is reviewed. In the last decade, there have been extensive developments in computational methods in response to the need for computer codes with which to study fundamental aerodynamic and aeroelastic problems in the critical transonic regime. For example, large commercial aircraft cruise most effectively in the transonic flight regime and computational fluid dynamics (CDF) provides a new tool, which can be used in combination with test facilities to reduce the costs, time, and risks of aircraft development. |
| File Size | 364864 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870007368 |
| Archival Resource Key | ark:/13960/t2x39p76g |
| Language | English |
| Publisher Date | 1987-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Test Facilities Transonic Flight Wings Supersonic Aircraft Computational Fluid Dynamics Coding Unsteady Aerodynamics Airfoils Unsteady Flow Aeroelasticity Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
