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Transonic unsteady aerodynamics and aeroelasticity 1987, part 1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1989 |
| Description | Computational fluid dynamics methods have been widely accepted for transonic aeroelastic analysis. Previously, calculations with the TSD methods were used for 2-D airfoils, but now the TSD methods are applied to the aeroelastic analysis of the complete aircraft. The Symposium papers are grouped into five subject areas, two of which are covered in this part: (1) Transonic Small Disturbance (TSD) theory for complete aircraft configurations; and (2) Full potential and Euler equation methods. |
| File Size | 25147478 |
| Page Count | 261 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890009863 |
| Archival Resource Key | ark:/13960/t4rj9bv8v |
| Language | English |
| Publisher Date | 1989-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aircraft Stability Transonic Flow Computational Fluid Dynamics Unsteady Aerodynamics Euler Equations of Motion Flow Distribution Aircraft Design Flutter Analysis Unsteady Flow Aeroelasticity Aircraft Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
