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Unsteady-pressure and dynamic-deflection measurements on an aeroelastic supercritical wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Eckstrom, Clinton V. Sandford, Maynard C. Seidel, David A. |
| Copyright Year | 1991 |
| Description | Transonic steady and unsteady pressure tests were conducted on a large elastic wing. The wing has a supercritical airfoil, a full span aspect ratio of 10.3, a leading edge sweepback angle of 28.8 degrees, and two inboard and one outboard trailing edge control surfaces. Only the outboard control surface was deflected statically and dynamically to generate steady and unsteady flow over the wing. The unsteady surface pressure and dynamic deflection measurements of this elastic wing are presented to permit correlations of the experimental data with theoretical predictions. |
| File Size | 98383031 |
| Page Count | 316 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920011412 |
| Archival Resource Key | ark:/13960/t6k120g9f |
| Language | English |
| Publisher Date | 1991-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Deflection Steady Flow Unsteady Flow Aspect Ratio Pressure Sweepback Control Surfaces Flow Distribution Trailing Edges Unsteady Aerodynamics Supercritical Wings Wing Profiles Aeroelasticity Leading Edges Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
