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Aeroelastic modeling of the active flexible wing wind-tunnel model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Heeg, Jennifer Bennett, Robert M. Silva, Walter A. |
| Copyright Year | 1991 |
| Description | The primary issues involved in the generation of linear, state-space equations of motion of a flexible wind tunnel model, the Active Flexible Wing (AFW), are discussed. The codes that were used and their inherent assumptions and limitations are also briefly discussed. The application of the CAP-TSD code to the AFW for determination of the model's transonic flutter boundary is included as well. |
| File Size | 875564 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910013020 |
| Archival Resource Key | ark:/13960/t5q86715g |
| Language | English |
| Publisher Date | 1991-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flexible Wings Unsteady Aerodynamics Wind Tunnel Tests Models Wind Tunnel Models Linear Equations Boundaries Equations of Motion Aeroelasticity Transonic Flutter Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
